Abstract

For large initial rectilinear displacements, we investigate free response of a linear oscillator inertially coupled to a rotational nonlinear energy sink (NES). Absent direct rectilinear damping, two ranges of orbitally stable solutions are accessible, in contrast to one range at lower, intermediate energies (2021, J. Appl. Mech. 88, 121009). As at lower initial energies, fractal and riddled basins of attraction are identified for both previously considered numerical combinations of the two dimensionless parameters (characterizing rotational damping, and coupling of rotational to rectilinear motion). In this case, however, the final amplitude, in addition to the final angular orientation, displays initial-condition sensitivity. For one parameter combination, most motionless initial conditions (MICs, with the masses of the linear oscillator and NES both initially at rest) lead to a discrete set of “special” orbitally stable solutions with one of two amplitudes, and no MICs lead to complete dissipation of initial energy. For the other combination, the results are similar to those at intermediate initial energies, with no MICs leading to special solutions, and many leading to complete dissipation. Results for both parameter combinations strongly suggest that no qualitatively new behavior occurs for initial energies beyond those considered here, with nonrotating asymptotic special-amplitude solutions having larger rectilinear amplitude either not existing or existing in only very small parts of the MIC space. With direct damping of rectilinear motion, transient chaos leads to initial-condition sensitivity of settling time, with the case of no direct rectilinear damping providing good guidance to damped-case behavior.

1 Introduction

We consider free response of a linearly sprung vibrating primary mass inertially coupled to a rotational nonlinear energy sink (NES). Coupling of rectilinear oscillation of the primary mass to viscously damped rotation of the NES mass about a vertical axis leads to targeted energy transfer (TET), in which vibrational energy of the primary mass is transferred to rotational energy of the NES mass, which is then dissipated. The nonlinear dynamics has been investigated numerically [15] and experimentally [1]. This approach to TET has been explored in simulations of structural vibration suppression [6] and flow-induced vibration suppression [710].

As discussed previously [15], the free response is governed by the dimensionless equations
(1a)
(1b)
subject to initial conditions
(2a)
(2b)
(2c)
and
(2d)
where η is the dimensionless rectilinear displacement (scaled with the distance from a rotating point mass to its axis of rotation), τ is the dimensionless time, and θ is the angular position (or “orientation”) of the rotating mass. Here, α, σ, and λ are a dimensionless rotational damping parameter, a mass ratio, and a dimensionless rectilinear damping parameter, respectively. Equations (1) and (2) also apply to a distributed mass rotating about a primary mass [7], and to a single mass allowed to rotate (with linear frictional damping) about a vertical axis (a) not passing through its center of mass and (b) connected by a linear spring to a foundation [4]. In those cases, σ more generally characterizes the strength of coupling between rectilinear and rotational motion.
Absent direct damping of rectilinear oscillation, Ding and Pearlstein [4] established that all asymptotic solutions of Eqs. 1(a) and 1(b) are of the form
(3)
where
(4a)
(4b)
(4c)

If B > 0, then θ = , where n is an integer [15], and we have a “semi-trivial” solution [11] of the type reported in early work [13]. There are also motionless (“zero-energy”) asymptotic solutions with B = 0 (and θ typically not an integer multiple of π) [4]. Floquet analysis [4] shows that the semi-trivial solutions are orbitally stable if B lies below a lowest critical value A0(α) or in a “tongue” A2k−1(α) < B < A2k(α), k = 1, 2, 3, …, whose extent decreases rapidly as k increases or as α decreases. For all other values of B, semi-trivial solutions are unstable.

For two numerical combinations of α and σ (including that focused on by Gendelman et al. [1] and Sigalov et al. [2,3]) with no rectilinear damping, we reported [4,5] a number of results not found in the previous work [13]. For 0 < ηiA0(α) and both (α, σ, λ) = (1, 0.01, 0) and (0.1, 0.1, 0), there is a wide and connected part of the motionless initial-condition (MIC) space (wherein νi = Ωi = 0) in which damped rotation of the NES mass dissipates all initial energy of the primary mass, giving a motionless final state [4]. For larger initial rectilinear displacements, in the range A0(α) ≤ ηiA1(α), results for (α, σ, λ) = (1, 0.01, 0) and (0.1, 0.1, 0) are quite different [5]. For (α, σ, λ) = (1, 0.01, 0), a wide and connected set of MICs lead to orbitally stable semi-trivial solutions with ηi-dependent asymptotic amplitudes just below A0(1), or for larger ηi in the range A0(1) ≤ ηiA1(1), to asymptotic solutions with ηi-invariant amplitude B∞,s,1 = 1.1712734… (with θ = for a range of integer n). We refer to the latter as “ground-state time-harmonic special solutions,” with a single value of B and different θ. For A0(1) ≤ ηiA1(1), no MICs were found for which all initial energy is dissipated. On the other hand, for (α, σ, λ) = (0.1, 0.1, 0) and A0(0.1) ≤ ηiA1(0.1), virtually all MICs lead to B < A0(0.1), a large fraction of MICs lead to complete dissipation, and no MICs leading to special solutions are found. Fractality and riddling of asymptotic solutions for both combinations in MIC space were characterized [5].

Here, we consider initial rectilinear displacements exceeding A1(α), the upper limit of oscillation amplitude of the first range of orbital instability, and show that Eqs. 1(a) and 1(b) support rich dynamical behavior not found earlier [15]. For (α, σ, λ) = (1, 0.01, 0), a wide range of MICs lead to a second set of time-harmonic “special” solutions, each with a different value of θ = , but all having the same amplitude within T1(1), giving rise to fractal and riddled basins of attraction. (In the second tongue of orbital stability, T2(1), there is also a set of time-harmonic special solutions with a single amplitude, but the range of MICs leading to them is very limited.) For (α, σ, λ) = (0.1, 0.1, 0), the rotational damping parameter is sufficiently small that the two lowest-lying tongues (see Fig. 1 of Ref. [4]) are very narrow. As a result, the only MICs approaching a semi-trivial solution in T1(0.1) lie in small, connected sets very close to θi = 0 or π, or are apparently isolated. No semi-trivial solutions are found with asymptotic amplitudes in T2(0.1). For all other initial angular positions, asymptotic behavior is qualitatively similar to that observed for smaller initial rectilinear displacements [5].

Fig. 1
Free response for (α, σ, λ) = (1, 0.01, 0). For (ηi, θi) = (4.43, 0.15π), time series of (a) η, (b) θ/π, (c) dθ/dτ, and (d) B. For (ηi, θi) = (4.5, 0.725π), time series of (e) η, (f) θ/π, (g) dθ/dτ, and (h) B. For (ηi, θi) = (11.2, 5 × 10−4π), time series of (i) η, (j) θ/π, (k) dθ/dτ, and (l) B. For (ηi, θi) = (11.21, 10−4π) integrated with δ = 10−12, time series of (m) η, (n) θ/π, and (o) dθ/dτ, (p) B. Horizontal dashed lines correspond to |η| = A2(1) in (a) and (e), B = A2(1) in (d) and (h), and |η| = A4(1) in (i) and (m).
Fig. 1
Free response for (α, σ, λ) = (1, 0.01, 0). For (ηi, θi) = (4.43, 0.15π), time series of (a) η, (b) θ/π, (c) dθ/dτ, and (d) B. For (ηi, θi) = (4.5, 0.725π), time series of (e) η, (f) θ/π, (g) dθ/dτ, and (h) B. For (ηi, θi) = (11.2, 5 × 10−4π), time series of (i) η, (j) θ/π, (k) dθ/dτ, and (l) B. For (ηi, θi) = (11.21, 10−4π) integrated with δ = 10−12, time series of (m) η, (n) θ/π, and (o) dθ/dτ, (p) B. Horizontal dashed lines correspond to |η| = A2(1) in (a) and (e), B = A2(1) in (d) and (h), and |η| = A4(1) in (i) and (m).
Close modal

The remainder of the paper is organized as follows. For (α, σ, λ) = (1, 0.01, 0), we briefly discuss representative trajectories in Sec. 2, followed in Sec. 3 by a discussion of two additional sets of time-harmonic special solutions. In Sec. 4, we divide the MIC space into regions according to asymptotic behavior of trajectories originating within those regions, and in Sec. 5 characterize fine-scale structure in the MIC space. In Sec. 6, we present results for (α, σ, λ) = (0.1, 0.1, 0), and in Sec. 7 consider direct damping of rectilinear oscillation of the primary mass for the two combinations of α and σ. A discussion and conclusions follow in Secs. 8 and 9.

2 Representative Trajectories for (α, σ, λ) = (1, 0.01, 0)

For (α, σ, λ) = (1, 0.01, 0), we will show in Sec. 5 that initial-condition sensitivity in broad portions of the MIC space leads to fractal or riddled basins for certain asymptotic solutions. Because initial-condition sensitivity gives rise to sensitivity with respect to numerical integration details [5,1216], we do not attempt to track the “exact” solution over an extended time interval using a higher-order accurate integrator, a small time-step size, and multiple precision arithmetic. Rather, we recognize that initial conditions cannot be precisely specified in experiments, and instead focus on understanding sensitivity and associating it with the underlying dynamics. All trajectories here are integrated using matlab subroutine ode45 with, as before [4,5], the absolute and relative error tolerances in this explicit (4,5) Runge–Kutta integrator taken to be equal, with their common value denoted by δ, equal to 10−8 unless otherwise stated. We use 64-bit arithmetic. The asymptotic B (sometimes zero) is extracted by closely following the method previously described [4] using the Levenberg–Marquardt algorithm [17] with 50 iterations. Wavelet transforms were performed as previously described [4,5].

For (α, σ, λ) = (1, 0.01, 0) with A1(1) ≤ ηi ≤ 15, a Floquet analysis [4] identified the three lowest ranges of oscillation amplitude in which semi-trivial solutions are orbitally stable. These are 0 ≤ B < A0(1), A1(1) < B < A2(1), and A3(1) < B < A4(1), with A0(1) = 1.18341…, A1(1) = 4.20291…, A2(1) = 4.40642…, A3(1) = 11.18428…, and A4(1) = 11.20204…. For ηi considered here, there exist MICs whose trajectories asymptotically approach solutions in each orbitally stable range. In addition to the countable set of ground-state time-harmonic special solutions with asymptotic amplitude B∞,s,1 = 1.1712734… (with members of the set having θ = for different integer n) [5], we find two additional sets of time-harmonic special solutions lying within T1(1) and T2(1), with asymptotic rectilinear amplitudes B∞,s,2 = 4.4056717… and B∞,s,3 = 11.2020156…, respectively, discussed in Sec. 3. Here, we discuss representative trajectories for (α, σ, λ) = (1, 0.01, 0), some of which show sensitivity of asymptotic amplitude to initial conditions, not found for 0 < ηi < A1(1) [4,5].

2.1 Cases Insensitive to Initial-Condition Disturbance and Integration Tolerance.

We first consider MICs for which the baseline (BL) trajectory computed with the default δ is graphically indistinguishable over 0 ≤ τ ≤ 2 × 104 from those computed when δ is reduced from 10−8 to 10−12, or ηi is increased by 10−8, referred to as the reduced integration tolerance (RIT) and perturbed initial-condition (PIC) trajectories, respectively.

Case 1. Capture inT1(1) withB < B∞,s,2: For (ηi, θi) = (4.43, 0.15π), Figs. 1(a)1(d) show a short irregular rotation between τ = 0 and 20, with significant variation of θ and B. For τ > 20, the angular velocity undergoes a decaying oscillation, and the trajectory asymptotes to harmonic rectilinear oscillation with (B, θ) = (4.386…, − 4π).

Case 2. Capture inT1(1) withB = B∞,s,2: Figures 1(e)1(h) show the trajectory for (ηi, θi) = (4.5, 0.725π). The rotation rate undergoes an irregular transient for 0 ≤ τ ≤ 25 (shown in detail in Figs. S1(a)–S1(f) available in the Supplemental Materials), followed by abrupt decay, by slow growth of its envelope to a local maximum near τ = 140, and by slow decay to zero (Fig. S1(g)), leading to (B, θ) = (4.4056717…, − 5π) with the amplitude of a time-harmonic special solution.

Case 3. Capture inT2(1) withB < B∞,s,3: For (ηi, θi) = (11.2, 5 × 10−4π), with θi ≈ 0, Figs. 1(i)1(l) show that energy dissipation is limited, with B lying within T2(1).

Case 4. Capture inT2(1) withB = B∞,s,3: For (ηi, θi) = (11.21, 10−4π), with ηi > A4(1) = 11.20204, Figs. 1(m)1(p) show that after initial energy transfer to the rotational mode, during which / increases to its maximum, 0.237, at τ = 68.53, rotational energy decays asymptotically to zero, but much more slowly than in Case 3. The difference in energy dissipation rate between this and Case 3 can be understood as follows. Figures S2(a)–S2(f) available in the Supplemental Materials show, in addition to trajectories for Cases 3 and 4, one for an “intermediate” MIC. Figure S2(c) available in the Supplemental Materials shows that for (ηi, θi) = (11.2, 10−4π), / decays quite rapidly, and with much greater similarity to Case 3 than to Case 4, showing that for those MICs giving rise to B within T2(1), decay of / is closely related to whether ηi lies within the orbitally stable range of rectilinear displacements, rather than to the closeness of θi to an integer multiple of π. (We used δ = 10−12 for Case 4, because over the very long time scale demanded by the weak decay, numerical error for δ = 10−8 leads to long-time linear decrease of B(τ) rather than asymptotic decay to B∞,s,3).

2.2 Cases Sensitive to Initial Conditions and Integration Tolerance.

Here we discuss two MICs for which transient chaos leads to initial-condition sensitivity of the asymptotic solutions. For these nominal MICs, we apply a wavelet transform to / and characterize the transient chaos by computing the correlation dimension, closely following procedures used earlier [4,5].

Case 5. Capture inT1(1) withB < B∞,s,2: For (ηi, θi) = (8.1, 0.7π), Figs. 2(a)2(c) show time series of the dynamical variables, while Fig. 2(d) shows a wavelet transform of /. In Figs. 2(b) and 2(d), we see that the NES mass undergoes fairly regular rotation over 0 ≤ τ ≤ 145, with significant energy at two frequencies (second and sixth harmonics f = 0.16 and 0.48, respectively, having a fundamental frequency f = 0.08; Fig. 2(d)). For 145 ≤ τ ≤ 655, the trajectory is more irregular (Fig. 2(b)), and the wavelet transform is broadband (Fig. 2(d)), suggesting chaotic behavior. Beyond τ = 655, the time series of / becomes more regular, with frequencies f = 0.08 and f = 0.40 (fifth harmonic) being the most prominent over the range 655 ≤ τ ≤ 824. Rotation is predominantly counterclockwise for 838 ≤ τ ≤ 879 and predominantly clockwise for 892 ≤ τ ≤ 918. During those intervals, the most energetic frequency is about 0.33 (fourth harmonic). Beyond τ = 920, / rapidly decays to zero (Fig. 2(b)), with (B, θ) = (4.384…, − 2π).

Fig. 2
For (ηi, θi) = (8.1, 0.7π) with (α, σ, λ) = (1, 0.01, 0), (a) time series of θ for 0 ≤ τ ≤ 1200; (b) time series of dθ/dτ for 0 ≤ τ ≤ 1200; (c) time series of B for 0 ≤ τ ≤ 1200; and (d) wavelet transform of dθ/dτ for 0 ≤ τ ≤ 1200. Horizontal dashed line corresponds to B = A2(1) in (c).
Fig. 2
For (ηi, θi) = (8.1, 0.7π) with (α, σ, λ) = (1, 0.01, 0), (a) time series of θ for 0 ≤ τ ≤ 1200; (b) time series of dθ/dτ for 0 ≤ τ ≤ 1200; (c) time series of B for 0 ≤ τ ≤ 1200; and (d) wavelet transform of dθ/dτ for 0 ≤ τ ≤ 1200. Horizontal dashed line corresponds to B = A2(1) in (c).
Close modal

For the same nominal MIC, Figs. S3(a)–S3(c) available in the Supplemental Materials show the sensitivity of the trajectories and asymptotic solutions if we reduce the integration tolerance δ from 10−8 to 10−12 (RIT case) or perturb ηi to 8.1 + 10−9 (PIC case). Time series of η(τ) for the RIT and PIC cases are graphically indistinguishable, with both leading to B = B∞,s,1, whereas B for the BL trajectory lies inside T1(1), just below B∞,s,2, showing that the asymptotic amplitude depends sensitively on initial conditions and integration details. Figures S3(b) and S3(c) available in the Supplemental Materials show that time series for θ/π are distinct for the BL, RIT, and PIC cases, as are those for /. The angular velocity (Fig. S3(c) available in the Supplemental Materials) is essentially identical for all three cases until about τ = 190 (including the beginning of transient chaos), beyond which trajectories begin to diverge. Wavelet transformation (Figs. S4(b), S4(d), and S4(f) available in the Supplemental Materials) shows that the frequency content in each case is very similar through the end of the second interval of transient chaos (ending near τ = 920). Beyond that time, the angular velocity in the BL case rapidly decays to zero, while in the RIT and PIC cases, the oppositely signed envelopes of / (Figs. S3(c), S4(c), and S4(e) available in the Supplemental Materials) correspond to nearly identical wavelet transformations, with the most energetic frequencies being about 0.17, 0.33, and 0.49. For the RIT and PIC cases, after the irregularity during 1470 ≤ τ ≤ 1680, the frequency content during oscillatory decay (1705 ≤ τ ≤ 2500) is dominated by f = 0.08 and 0.24. For each trajectory during each chaotic transient, we calculated the correlation dimension dcorr [5], taken as the limiting value for embedding dimensions up to and including 56. For 200 ≤ τ ≤ 600, the BL, RIT, and PIC trajectories give dcorr = 2.28, 2.27, and 2.48, respectively. Later intervals of irregular behavior coincide for the RIT and PIC trajectories, giving dcorr = 2.98 and 3.02, respectively, over 835 ≤ τ ≤ 960, and 4.22 and 3.77, respectively, over 1500 ≤ τ ≤ 1680. That these values all exceed 2.0 and are in each interval in good agreement, even over the latter two intervals whose shortness (about 20 and 35 oscillations, respectively) complicates extraction of an accurate dcorr, indicates that the irregularity is due to transient chaos.

Case 6. Capture inT1(1) withB = B∞,s,2: For (ηi, θi) = (7.5, 0.4π), Figs. 3(a)3(d) show that the motion undergoes an irregular transient for 0 ≤ τ ≤ 820, beyond which B and θ rapidly approach their asymptotes. The envelope of / then grows slowly until τ = 870, after which it slowly decays to zero. The asymptotic solution is (B, θ) = (4.4056717…, − 13π), with amplitude B∞,s,2 lying just below A2(1), the upper bound of the first tongue of stability. Analogous to the ground-state time-harmonic special solutions [5] giving rise to B = B∞,s,1, the special amplitude B∞,s,2 is the single limiting asymptotic amplitude of a large fraction of MICs (Sec. 3). Trajectories for the BL, RIT, and PIC cases integrated with (ηi, θi, δ) = (7.5, 0.4π, 10−8), (7.5, 0.4π, 10−12), and (7.5 + 10−8, 0.4π, 10−8), respectively, show that the rectilinear displacements of the BL and RIT trajectories are graphically indistinguishable (Fig. S5(a) available in the Supplemental Materials), with asymptotic amplitude B∞,s,2, whereas the PIC case has asymptotic amplitude B∞,s,1. On the other hand, θ and / for the three trajectories diverge near τ = 76 (Figs. S5(b) and S5(c) available in the Supplemental Materials), and η diverges near τ = 740 (Fig. S5(a) available in the Supplemental Materials), leading to three different combinations (B, θ), again indicating sensitivity with respect to integration tolerance and initial conditions.

Fig. 3
For (ηi, θi) = (7.5, 0.4π) with (α, σ, λ) = (1, 0.01, 0), (a) time series of θ for 0 ≤ τ ≤ 1200; (b) time series of dθ/dτ for 0 ≤ τ ≤ 1200; (c) time series of B for 0 ≤ τ ≤ 1200; and (d) wavelet transform of dθ/dτ for 0 ≤ τ ≤ 1200. Horizontal dashed line corresponds to B = A2(1) in (c).
Fig. 3
For (ηi, θi) = (7.5, 0.4π) with (α, σ, λ) = (1, 0.01, 0), (a) time series of θ for 0 ≤ τ ≤ 1200; (b) time series of dθ/dτ for 0 ≤ τ ≤ 1200; (c) time series of B for 0 ≤ τ ≤ 1200; and (d) wavelet transform of dθ/dτ for 0 ≤ τ ≤ 1200. Horizontal dashed line corresponds to B = A2(1) in (c).
Close modal

3 Two Additional Sets of Time-Harmonic Special Solutions for (α, σ, λ) = (1, 0.01, 0)

As discussed in Ref. [5], there is a large, connected range of MICs lying below A1(1) = 4.20291… for which the asymptotic rectilinear amplitude is B∞,s,1 = 1.1712734…, just below A0(1) = 1.18341…. Here, we discuss two other sets of time-harmonic special solutions with amplitudes B∞,s,2 = 4.4056717… and B∞,s,3 = 11.2020156…, lying just below A2(1) = 4.40642… and A4(1) = 11.20204…, respectively.

For A1(1) ≤ ηi ≤ 4.6 and θi near 0 or π, B depends continuously on MICs in two connected parts of MIC space, qualitatively similar to Regions IIA and IIB [4,5]. There is a range of MICs (Fig. 4(a)) with ηi lying just above A2(1) and with θi near zero, for which the limiting behavior is BB∞,s,2 as ηi increases, similar to the limit BB∞,s,1 as ηi increases just above A0(1) [5]. To further verify that B∞,s,2 is a single value rather than a narrow range, Table 1 provides statistics (mean, variance, and difference between maximum and minimum) for amplitudes of the T1(1) time-harmonic special solution, B∞,s,2, for 243 MICs shown in Table S1(a) available in the Supplemental Materials lying within 4.42 ≤ ηi ≤ 4.5 with θi = 10−3π, 5 × 10−4π, and 10−4π, each integrated with δ = 10m, for 8 ≤ m ≤ 12, and extrapolated to large m using Shanks' transformation [18], as in Ref. [5]. As the integration tolerance is tightened, the values of B lie in an increasingly narrow range, corresponding to a well-defined limiting value of B∞,s,2 = 4.4056717… (Table 1), analogous to the value (1.1712734…) determined earlier for B∞,s,1 [5].

Fig. 4
For (α, σ, λ) = (1, 0.01, 0), (a) B∞ approaching B∞,s,2 = 4.4056717… for increasing ηi integrated with δ = 10−8. θi = 10−4π, dots; θi = 5 × 10−4π, solid line; θi = 10−3π, dash-dotted line. (b) B∞ approaching B∞,s,3 = 11.2020156… for increasing ηi integrated with δ = 10−12. θi = 10−5π, dots; θi = 5 × 10−5π, solid line; θi = 10−4π, dash-dotted line. In (a), horizontal and vertical dashed lines correspond to B∞ = A2(1) and ηi = A2(1), respectively. In (b), horizontal and vertical dashed lines correspond to B∞ = A4(1) and ηi = A4(1), respectively.
Fig. 4
For (α, σ, λ) = (1, 0.01, 0), (a) B∞ approaching B∞,s,2 = 4.4056717… for increasing ηi integrated with δ = 10−8. θi = 10−4π, dots; θi = 5 × 10−4π, solid line; θi = 10−3π, dash-dotted line. (b) B∞ approaching B∞,s,3 = 11.2020156… for increasing ηi integrated with δ = 10−12. θi = 10−5π, dots; θi = 5 × 10−5π, solid line; θi = 10−4π, dash-dotted line. In (a), horizontal and vertical dashed lines correspond to B∞ = A2(1) and ηi = A2(1), respectively. In (b), horizontal and vertical dashed lines correspond to B∞ = A4(1) and ηi = A4(1), respectively.
Close modal
Table 1

Statistics of B for (α, σ, λ) = (1, 0.01, 0) and 4.42 ≤ ηi ≤ 4.5 with θi = 10−3π, θi = 5 × 10−4π, and θi = 10−4π with δ = 10m (8 ≤ m ≤ 12). In the bottom row, a second-order Shanks transformation [18] was applied to the values of B at each of the 243 MICs to estimate B as m → ∞. These 243 extrapolates were then used to calculate the mean, variance, and B∞,maxB∞,min

MeanVarianceB∞,maxB∞,min
δ = 10−84.405652218197022.1648 × 10−131.8322 × 10−6
δ = 10−94.405669850470992.0831 × 10−151.7970 × 10−7
δ = 10−104.405671579086822.0317 × 10−171.7737 × 10−8
δ = 10−114.405671749752881.9975 × 10−191.7501 × 10−9
δ = 10−124.405671766680451.9624 × 10−211.6800 × 10−10
S2(B)4.405671768550942.4455 × 10−241.5020 × 10−11
MeanVarianceB∞,maxB∞,min
δ = 10−84.405652218197022.1648 × 10−131.8322 × 10−6
δ = 10−94.405669850470992.0831 × 10−151.7970 × 10−7
δ = 10−104.405671579086822.0317 × 10−171.7737 × 10−8
δ = 10−114.405671749752881.9975 × 10−191.7501 × 10−9
δ = 10−124.405671766680451.9624 × 10−211.6800 × 10−10
S2(B)4.405671768550942.4455 × 10−241.5020 × 10−11

Figures 1(i)1(p) also show that trajectories emanating within or slightly above T2(1) with θi close to an integer multiple of π lead to values of B lying in T2(1), with almost no energy dissipation. As with ηi values just above either A0(1) or A2(1) giving rise to time-harmonic special solutions, having B = B∞,s,1 or B∞,s,2, respectively, here there exist connected MIC regions, above A4(1), corresponding to a new set of time-harmonic special solutions, with B = B∞,s,3 = 11.2020156… (Table 2, and Table S1(b) available in the Supplemental Materials), lying within T2(1). Figure 4(b) shows that B approaches B∞,s,3 for θi near zero. For 23 ηi values within 11.208 < ηi < 11.219 with θi = 10−4π, 5 × 10−5π, and 10−5π, statistics for 69 trajectories shown in Table 2 suggest that B∞,s,3 is a single limiting value, and does not correspond to a narrow range of nonzero extent.

Table 2

Statistics of B for (α, σ, λ) = (1, 0.01, 0) and 11.208 ≤ ηi ≤ 11.219 with θi = 10−4π, θi = 5 × 10−5π, and θi = 10−5π with δ = 10m (8 ≤ m ≤ 12). In the bottom row, a second-order Shanks transformation [18] was applied to the values of B at each of the 69 MICs to estimate B as m → ∞. These 69 extrapolates were then used to calculate the mean, variance, and B∞,maxB∞,min

MeanVarianceB∞,maxB∞,min
δ = 10−811.20195831882047.7713 × 10−112.9115 × 10−5
δ = 10−911.20201031673127.4332 × 10−132.8602 × 10−6
δ = 10−1011.20201512790317.8246 × 10−152.9613 × 10−7
δ = 10−1111.20201559662991.5995 × 10−164.4391 × 10−8
δ = 10−1211.20201564290622.9685 × 10−171.9577 × 10−8
S2(B)11.20201564799742.2230 × 10−171.6874 × 10−8
MeanVarianceB∞,maxB∞,min
δ = 10−811.20195831882047.7713 × 10−112.9115 × 10−5
δ = 10−911.20201031673127.4332 × 10−132.8602 × 10−6
δ = 10−1011.20201512790317.8246 × 10−152.9613 × 10−7
δ = 10−1111.20201559662991.5995 × 10−164.4391 × 10−8
δ = 10−1211.20201564290622.9685 × 10−171.9577 × 10−8
S2(B)11.20201564799742.2230 × 10−171.6874 × 10−8

As mentioned in Ref. [5], the mechanism by which each of a large number of MICs leads to an orbitally (but not asymptotically) stable time-harmonic solution with a single rectilinear amplitude involves a countable set of attracting manifolds, each leading to an orbitally stable solution with precisely one amplitude, but different θ. For the special solutions with B = B∞,s,2 and B∞,s,3, these attracting manifolds lie in parts of the phase space where the energy E (defined in Eq. (5) of Ref. [4]) exceeds [A2(1)]2/2 and [A4(1)]2/2, respectively. The details of these manifolds are beyond the scope of this work.

4 Partitioning The Motionless Initial-Condition Space and Basins of Attraction for (α, σ, λ) = (1, 0.01, 0)

For both combinations of α and σ and smaller initial energies [4,5], there are three regions in the MIC space (Regions I, IIA, and IIB) in which B and θ vary continuously, with the behavior becoming fractal or riddled for larger initial energies (in Region III). For (α, σ, λ) = (1, 0.01, 0), results in Region III show that θ (but not B) is sensitive to initial conditions, and there is a large connected portion of MIC space corresponding to the single limiting rectilinear amplitude B∞,s,1 = 1.1712734…., with no zero-energy solutions being found.

For (α, σ, λ) = (1, 0.01, 0), we show in Secs. 4.1 and 4.2 that at larger initial energies, the asymptotic amplitude B also becomes sensitive to initial conditions, and identify two additional regions (Region IV; separated by ηi = A1(1) from Region III; and Region V, separated by ηi = A2(1) from Region IV; in both cases as shown in Fig. 5(a)) in the MIC space. In Region IV, most MICs lead to the ground-state time-harmonic special solution with asymptotic amplitude B = B∞,s,1, while the remainder lead to solutions having A1(1) < B < A2(1). Region V includes MICs leading to special solutions having two other amplitudes, namely, B = B∞,s,2 and B∞,s,3, with the latter approached only for a narrow range of MICs, unlike the former, which is reached by a wide range of MICs. Like solutions with asymptotic amplitude B∞,s,1, these additional special solutions have amplitudes in ranges of orbital stability established by the linear stability analysis [4]. We also show (see details in Sec. 4.2) that additional ranges of orbitally stable semi-trivial solutions at still higher amplitudes are so narrow that very few MICs are led to them.

Fig. 5
Schematic (not to scale) showing Regions I, IIA, IIB, III, IV, and V for (a) (α, σ, λ) = (1, 0.01, 0) and (b) (α, σ, λ) = (0.1, 0.1, 0). In (a) and (b), Region V and Region III, respectively, extend beyond the range of ηi considered.
Fig. 5
Schematic (not to scale) showing Regions I, IIA, IIB, III, IV, and V for (a) (α, σ, λ) = (1, 0.01, 0) and (b) (α, σ, λ) = (0.1, 0.1, 0). In (a) and (b), Region V and Region III, respectively, extend beyond the range of ηi considered.
Close modal

4.1 Partitioning of the Motionless Initial-Condition Space.

For 736 MICs over 1.64 ≤ ηi ≤ 15 and 0 < θi < π, Figs. 6 and 7 show values of B and θ, respectively. For these and 4619 additional MICs in this range of ηi, distributions of B and θ (Tables S2(a) and S2(b) available in the Supplemental Materials, respectively) reveal no trajectory for which all initial energy is dissipated and show that BB∞,s,1 = 1.1712734…. For 4.20291… = A1(1) ≤ ηiA2(1) = 4.40642…, Figs. 6 and 7 show that MICs for which BB∞,s,1 are concentrated near θi = 0 and π and lead to solutions having A1(1) ≤ BA2(1), with θ being the integer multiple of π nearest to θi. In this range of ηi, the remaining MICs, for which BB∞,s,1, are apparently scattered throughout A1(1) ≤ ηiA2(1) (e.g., (ηi, θi) = (4.34, 0.425π)), with −9πθ ≤ 3π (Tables S2(a) and S2(b) available in the Supplemental Materials).

Fig. 6
For (α, σ, λ) = (1, 0.01, 0), variation of B∞ for 1.64 ≤ ηi ≤ 15 with nonuniformly incremented ηi and θi, taken from Table S2(a) available in the Supplemental Materials, which shows values for 5355 initial conditions, with more significant digits for B∞. B∞ = B∞,s,1, orange; B∞ = B∞,s,2, gray; A1(1) ≤ B∞ < B∞,s,2, blue; B∞,s,2 < B∞ ≤ A2(1), yellow; A3(1) ≤ B∞ ≤ A4(1), red
Fig. 6
For (α, σ, λ) = (1, 0.01, 0), variation of B∞ for 1.64 ≤ ηi ≤ 15 with nonuniformly incremented ηi and θi, taken from Table S2(a) available in the Supplemental Materials, which shows values for 5355 initial conditions, with more significant digits for B∞. B∞ = B∞,s,1, orange; B∞ = B∞,s,2, gray; A1(1) ≤ B∞ < B∞,s,2, blue; B∞,s,2 < B∞ ≤ A2(1), yellow; A3(1) ≤ B∞ ≤ A4(1), red
Close modal
Fig. 7
For (α, σ, λ) = (1, 0.01, 0), variation of θ∞ for 1.64 ≤ ηi ≤ 15 with nonuniformly incremented ηi and θi, taken from Table S2(b) available in the Supplemental Materials on the ASME Digital Collection, which shows values for 5355 initial conditions. Yellow and green backgrounds denote θ∞/π = 0 and θ∞/π = 1, respectively. Other values of θ∞/π, all integers, are shown in black (θ∞/π > 1) or blue (θ∞/π < 0), with the false-color background corresponding to the magnitude of θ∞/π.
Fig. 7
For (α, σ, λ) = (1, 0.01, 0), variation of θ∞ for 1.64 ≤ ηi ≤ 15 with nonuniformly incremented ηi and θi, taken from Table S2(b) available in the Supplemental Materials on the ASME Digital Collection, which shows values for 5355 initial conditions. Yellow and green backgrounds denote θ∞/π = 0 and θ∞/π = 1, respectively. Other values of θ∞/π, all integers, are shown in black (θ∞/π > 1) or blue (θ∞/π < 0), with the false-color background corresponding to the magnitude of θ∞/π.
Close modal

Trajectories emanating from MICs close to θi = 0 or π undergo initially rapid growth in |/|. This is followed by an interval of relatively slow decay, before approaching a non − B∞,s,1 solution, with θ being the integer multiple of π nearest to θi, as illustrated for (ηi, θi) = (4.4, 0.001π) in Figs. 8(a) and 8(b). For these MICs, the NES mass rotates about θi and then settles to θ = 0 or π. No transient chaos is observed in /, whose relatively small magnitude (Fig. 8(b)) limits energy dissipation. This differs markedly from the situation for 1.64 ≤ ηiA1(1), where MICs near θi = 0 or π cannot “settle” into a nonrotating asymptotic state without rotationally dissipating enough energy (during transient chaos) to fall below B = A0(1). On the other hand, trajectories emanating from apparently isolated MICs giving rise to non − B∞,s,1 solutions undergo only a few irregular rotations before approaching their asymptotes, as shown in Figs. 8(c) and 8(d) for (ηi, θi) = (4.34, 0.425π). The short duration of rotational motion means that very little initial energy is dissipated, and the magnitude of θ is small. Compared with Fig. 8(b), Fig. 8(d) shows a much shorter duration of rotation, with greater variation in rotational rate. In both cases, the magnitude of θ is small, with limited dissipation of initial energy.

Fig. 8
For (α, σ, λ) = (1, 0.01, 0) with (ηi, θi) = (4.4, 0.001π), time series of (a) θ/π and (b) dθ/dτ. For (α, σ, λ) = (1, 0.01, 0) with (ηi, θi) = (4.34, 0.425π), time series of (c) θ/π and (d) dθ/dτ.
Fig. 8
For (α, σ, λ) = (1, 0.01, 0) with (ηi, θi) = (4.4, 0.001π), time series of (a) θ/π and (b) dθ/dτ. For (α, σ, λ) = (1, 0.01, 0) with (ηi, θi) = (4.34, 0.425π), time series of (c) θ/π and (d) dθ/dτ.
Close modal

For A2(1) ≤ ηi ≤ 15, Fig. 6 shows that the distribution of B is more complicated, with most MICs leading to (B∞,s,1, ) or (B∞,s,2, ), with the latter becoming dominant as ηi increases. There are also small ranges of (ηi, θi) for which the asymptotic solution is (B, ) with A1(1) < B < B∞,s,2, B∞,s,2 < B < A2(1), or A3(1) < B < A4(1). The significant dependence of B on ηi shown in Fig. 6 leads us to identify regions of MIC space exhibiting distinct distributions of asymptotic amplitudes, corresponding to A1(1) ≤ ηiA2(1) (Region IV), and A2(1) < ηi ≤ 15 (Region V), as shown in Figs. 9(a)9(c). (As discussed below, the upper limit shown for Region V is not a critical value beyond which the trajectories exhibit qualitatively different behavior.)

Fig. 9
Distribution of B∞ for all 5355 MICs in Tables S2(a) and S2(b) available in the Supplemental Materials is shown in (a), including Region III (over 1.64 ≤ ηi ≤ A1(1) = 4.2029…), Region IV (over A1(1) < ηi ≤ A2(1) = 4.4064…), and Region V (over ηi > A2(1)). Enlargement of B∞ distributions near T1(1) and T2(1) are shown in (b) and (c), respectively. B∞ = B∞,s,1, orange; B∞ = B∞,s,2, gray; A1(1) < B∞ < B∞,s,2, blue; B∞,s,2 < B∞ < A2(1), black; and 11.18428… = A3(1) < B∞ < A4(1) = 11.20204…, red.
Fig. 9
Distribution of B∞ for all 5355 MICs in Tables S2(a) and S2(b) available in the Supplemental Materials is shown in (a), including Region III (over 1.64 ≤ ηi ≤ A1(1) = 4.2029…), Region IV (over A1(1) < ηi ≤ A2(1) = 4.4064…), and Region V (over ηi > A2(1)). Enlargement of B∞ distributions near T1(1) and T2(1) are shown in (b) and (c), respectively. B∞ = B∞,s,1, orange; B∞ = B∞,s,2, gray; A1(1) < B∞ < B∞,s,2, blue; B∞,s,2 < B∞ < A2(1), black; and 11.18428… = A3(1) < B∞ < A4(1) = 11.20204…, red.
Close modal

Figure 10(a) shows how θ depends on ηi for 5355 MICs in Table S2(b) available in the Supplemental Materials, with Figs. 10(b) and 10(c) providing more detail for 4.2 ≤ ηi ≤ 4.6 and 11.17 ≤ ηi ≤ 11.25, respectively. Points are colored according to B values (Table S2(a) available in the Supplemental Materials), with the overwhelming majority being B = B∞,s,1 (orange) or B∞,s,2 (gray), and the remainder lying in the ranges shown in the figure caption. Variation of θ for 1.6 ≤ ηi ≤ 4.2 was discussed earlier [5]. For larger initial displacements lying within T1(1) (Region IV; see Figs. 9(a)9(c)), 888 of 1035 MICs lead to B = B∞,s,1 with 146πθ ≤ 174π or −178πθ ≤ −145π, and 147 MICs lead to A1(1) < B < A2(1) with θ = for much smaller values of |n| (Fig. 10(b)). For A2(1) < ηi ≤ 4.6, 231 of 360 MICs lead to B = B∞,s,1 and the others to A1(1) < B < A2(1). In the latter case, |θ| is relatively small, with the range widening as ηi increases. For 4.6 < ηi ≤ 15, 1424 of 2160 trajectories lead to B = B∞,s,2 with −45πθ ≤ 50π (Fig. 10(a)), and 674 to B = B∞,s,1 with 94πθ ≤ 217π or −213πθ ≤ −111π. Fifty-one other MICs have A1(1) < B < B∞,s,2 or B∞,s,2 < B < A2(1), and 11 (all with ηi lying in or slightly above T2(1), with θi close to 0 or π) have B within T2(1), with θ = 0 or π. (Note that B = B∞,s,3 for none of the MICs considered.)

Fig. 10
Distribution of θ∞ for (α, σ, λ) = (1, 0.01, 0) with (a) all 5355 MICs in Tables S2(a) and S2(b) available in the Supplemental Materials, over 1.64 ≤ ηi ≤ 15, (b) A1(1) ≤ ηi ≤ 4.6, and (c) 11.18 ≤ ηi ≤ 11.25. Color scheme as in Fig. 9: B∞ = B∞,s,1, orange; B∞ = B∞,s,2, gray; 4.20291… = A1(1) < B∞ < B∞,s,2 = 4.4056717…, blue; B∞,s,2 < B∞ < A2(1) = 4.40642…, black; and 11.18428… = A3(1) < B∞ < A4(1) = 11.20204…, red. Dashed lines mark boundaries of tongues T1(1) and T2(1). In (a), the width of T2(1) is so small that its boundaries appear as one.
Fig. 10
Distribution of θ∞ for (α, σ, λ) = (1, 0.01, 0) with (a) all 5355 MICs in Tables S2(a) and S2(b) available in the Supplemental Materials, over 1.64 ≤ ηi ≤ 15, (b) A1(1) ≤ ηi ≤ 4.6, and (c) 11.18 ≤ ηi ≤ 11.25. Color scheme as in Fig. 9: B∞ = B∞,s,1, orange; B∞ = B∞,s,2, gray; 4.20291… = A1(1) < B∞ < B∞,s,2 = 4.4056717…, blue; B∞,s,2 < B∞ < A2(1) = 4.40642…, black; and 11.18428… = A3(1) < B∞ < A4(1) = 11.20204…, red. Dashed lines mark boundaries of tongues T1(1) and T2(1). In (a), the width of T2(1) is so small that its boundaries appear as one.
Close modal

For (α, σ, λ) = (1, 0.01, 0), Tables S3(a) and S3(b) available in the Supplemental Materials show, analogously to Tables S2(a) and S2(b) available in the Supplemental Materials, the dependence of B and θ on MICs for δ = 10−10. For ηi ≤ 4.45, the values of B are essentially identical for δ = 10−8 and 10−10, even in parts of Region IV where B values lie in T1(1), sometimes at apparently isolated MICs. For all ηi ≤ 1.7, θ is the same for both values of δ, as discussed previously for ηi ≤ 1.64 [5]. In regions of MIC space where B or θ is sensitive to δ, general trends of asymptotic states are qualitatively similar for both δ values (e.g., |θ| increases with increasing ηi in Regions III and IV, with the MIC dependence of B and θ becoming more complex in Region V). Consistency of values and trends of asymptotic states for two values of δ strongly suggests that irregularity in the results is a property of the dynamical system, rather than an artifact of numerical integration.

4.2 Basins of Attraction.

For (α, σ, λ) = (1, 0.01, 0), we found that (B, θ) is a continuous function of ηi and θi in some regions of the MIC space (e.g., in Region I, where B = 0 and θ depends on ηi and θi, and in Regions IIA and IIB, where θ = 0 or π and B depends on ηi and θi) [4]. In those cases, there is, at best, a curve (rather than a basin) in the MIC space from which trajectories lead to a particular asymptotic solution, the number of final states is not countable, and the concept of a basin of attraction is not meaningful.

As discussed in Sec. 3 and shown in Fig. 9(a), a large fraction of MICs lead to time-harmonic special solutions with a small number of asymptotic rectilinear amplitudes, namely, B∞,s,1, B∞,s,2, or B∞,s,3, in each case with θ equal to an integer multiple of π, and with dynamical characteristics (e.g., energy, stability) depending only on the rectilinear amplitude. These solutions thus constitute a set for which the number of asymptotic solutions is countable, and for which the basins of attraction can be characterized.

In applications, B is likely to be of greater interest than θ. Thus, if nearby MICs have different asymptotic solutions, we will want to know if all have the same B, and differ only in the multiple of π in θ. To address this, we introduced the concepts of (a) “true basins of attraction” [5] for the set of MICs giving rise to a solution (B, ) for a particular combination of and B, and (b) “amplitude-only basins of attraction” for the union of MICs giving rise to one value of B regardless of θ.

The amplitude-only basin for solutions with B∞,s,3 = 11.2020156… is confined to small portions of MIC space slightly above the second tongue near (ηi, θi) = (B∞,s,3, 0) and (B∞,s,3, π), unlike at smaller ηi where a broad range of MICs lying above T1(1) lead to B = B∞,s,2. The range of MICs leading to solutions with B in the third tongue, T3(1), 21.507875… = A5(1) ≤ BA6(1) = 21.509052… (whose limits we determined by a Floquet analysis identical to that performed earlier [4]), is even smaller. The few MICs leading to solutions with BB∞,s,1 and B not lying within T1(1) are confined to an exceedingly narrow range of ηi in or slightly above the third tongue and to values of θi exceedingly close to an integer multiple of π (Table S4 available in the Supplemental Materials). (No MICs lying within or above T3(1) are found to lead to B within T2(1).)

Defining the tongue width w(Tk(α)) = A2k(α) − A2k−1(α), we see that w(T3(1)) = 1.18 × 10−3 is much less than w(T2(1)) = 1.78 × 10−2 and w(T1(1)) = 0.204. Progressive narrowing of these tongues of orbital stability as amplitude increases coincides with narrowing of the two ranges of θi (near 0 and π) for which an MIC can lead to B lying within that tongue. This shows that, except for MICs in progressively minute regions near an integer multiple of π within or above progressively narrow tongues of asymptotic amplitude, no MIC leads to an asymptotic state with B > A2(1). These results lead us to conclude that semi-trivial solutions within the second and third tongues of orbital stability identified by the Floquet analysis are unstable (by a nonlinear mechanism) when subjected to very small but noninfinitesimal angular disturbances.

For (α, σ, λ) = (1, 0.01, 0), these results show that, except in exceedingly narrow parts of the MIC space, MICs with even higher energy will have asymptotic rectilinear amplitudes in the same ranges as the MICs considered here.

5 Characterization of Fine-Scale Structure in The Motionless Initial-Condition Space for (α, σ, λ) = (1, 0.01, 0)

As discussed in Sec. 4.1, (a) BB∞,s,1 for several scattered MICs in Region IV and (b) the dependence of B on ηi and θi in Region V is complicated. For ensembles of trajectories, we show here that these scattered MICs are associated with absence of transient chaos in narrow parts of MIC space, where trajectories are invariant to MIC perturbation and integration tolerance. In contrast, complicated dependence of B on ηi and θi in Region V is associated with “riddled” behavior of amplitude-only basins of attraction, corresponding to initial-condition sensitivity mediated by transient chaos. While these behaviors seem to be qualitatively similar, the underlying mechanisms differ in Regions IV and V, as discussed in Secs. 5.1 and 5.2.

5.1 Bands in Region IV and Region V.

As shown in Fig. 6 and Table S2(a) available in the Supplemental Materials, apparently isolated MICs in Region IV lead to non − B∞,s,1 values of B lying in T1(1), surrounded by MICs leading to B = B∞,s,1. More detailed examination shows that the non − B∞,s,1 MICs are not isolated and instead exist within thin bands in the MIC space wherein all asymptotic solutions have non − B∞,s,1 amplitudes lying in T1(1). For the MIC rectangle (4.32 ≤ ηi ≤ 4.50, 0.35πθi ≤ 0.45π), Fig. 11(a) shows that (ηi, θi) = (4.34, 0.425π), which in Fig. 6 appears to be an isolated MIC leading to a non − B∞,s,1 solution, instead lies on a “primary band” extending from ηi just below 4.34, up into Region V. Within this band of MICs, all values of B lie in T1(1) and B appears to be a continuous function of ηi and θi, approaching B∞,s,2 = 4.4056717… in both the left and right “branches” as ηi ≈ 4.48 is reached in Region V. All MICs lying within this primary band have the asymptotic orientation θ = 6π. As discussed in Sec. 4.1, the only MICs leading to asymptotic trajectories with B = B∞,s,2 are either (a) close to θi = 0 or π with A1(1) < ηi < A2(1), for which B varies continuously between A1(1) and A2(1), and B = B∞,s,2 only on a curve in this part of MIC space, or (b) above Region IV, and hence with ηi above T1(1).

Fig. 11
For (α, σ, λ) = (1, 0.01, 0), B∞ distribution (a) in a band passing (ηi, θi) = (4.34, 0.425π); (b) enlargement of (a) within the left branch of the band, where B∞ approaches B∞,s,2; and (c) enlargement of (b). In (a–c), B∞ = B∞,s,1, orange; B∞ = B∞,s,2, gray; and B∞ lying within T1(1) with B∞ ≠ B∞,s,2, upper false-color scale for (a) and lower scale for (b and c). Regions IV and V are, respectively, below and above the horizontal line ηi = A2(1) = 4.40642….
Fig. 11
For (α, σ, λ) = (1, 0.01, 0), B∞ distribution (a) in a band passing (ηi, θi) = (4.34, 0.425π); (b) enlargement of (a) within the left branch of the band, where B∞ approaches B∞,s,2; and (c) enlargement of (b). In (a–c), B∞ = B∞,s,1, orange; B∞ = B∞,s,2, gray; and B∞ lying within T1(1) with B∞ ≠ B∞,s,2, upper false-color scale for (a) and lower scale for (b and c). Regions IV and V are, respectively, below and above the horizontal line ηi = A2(1) = 4.40642….
Close modal

Figure 11(b) expands the view of part of the MIC space (4.478 ≤ ηi ≤ 4.490, 0.3584πθi ≤ 0.3614π) shown in Fig. 11(a). This includes the part of the left branch within which B generally increases with increasing ηi and decreasing θi, and then assumes a constant value B∞,s,2, visible in gray in Figs. 11(b) and 11(c). This transition involves internal structure within the band, and considerable dependence of B on a direction “transverse” to the band. Recalling that MICs lying outside the band approach asymptotic solutions with B = B∞,s,1, it is clear that as one traverses the band (e.g., by increasing ηi and θi), MICs lead to asymptotic solutions with B = B∞,s,1 followed by A1(1) < B < A2(1), and then B = B∞,s,1.

Figure 11(c) expands the view of part of the MIC space (4.482 ≤ ηi ≤ 4.488, 0.3589πθi ≤ 0.3604π) shown in Fig. 11(b). For 0.3602πθi ≤ 0.3604π, the maximum values of B occur near the center of the band, while for 0.3589πθi ≤ 0.3602π, multiple local maxima of B are observed in the primary band. Figure 12 shows B as a function of ηi on two parallel lines
(5a)
(5b)
denoted by Lc (near the center of the band) and Lu (near the upper boundary of the band), respectively, both nearly parallel to the primary band. For MICs along Lc, B increases linearly as ηi increases, passes through a weak maximum near ηi = 4.4864, and then decreases slightly to B∞,s,2. Along Lu, B increases nearly linearly, passes through a more pronounced maximum near ηi = 4.4826 and then decreases to B∞,s,2. The nature of these two approaches to B∞,s,2 is qualitatively similar to the approach to B∞,s,1 in Region IIA and IIB [5], and to the approach to B∞,s,2 shown in Fig. 4(a). In all cases, there is a region of MIC space in which all values of B correspond to time-harmonic solutions with a single amplitude.
Fig. 12
For (α, σ, λ) = (1, 0.01, 0), variation of B∞ along Lu (see Fig. 11): ηi = −3.3803(θi/π − 0.3619) + 4.4773 (solid line); and along Lc (see Fig. 11): ηi = −3.3803(θi/π − 0.3619) + 4.4770 (dashed). The common asymptote of these two curves is B∞,s,2.
Fig. 12
For (α, σ, λ) = (1, 0.01, 0), variation of B∞ along Lu (see Fig. 11): ηi = −3.3803(θi/π − 0.3619) + 4.4773 (solid line); and along Lc (see Fig. 11): ηi = −3.3803(θi/π − 0.3619) + 4.4770 (dashed). The common asymptote of these two curves is B∞,s,2.
Close modal

Figure 11(a) also shows secondary bands with finer scales, depicted by a series of points, lying on curves locally parallel to the primary band. Details of one secondary band are shown in Fig. S6 available in the Supplemental Materials. For MICs lying in this secondary band (shown as green points), θ = −7π. Near this secondary band but not within it, we find six apparently isolated points for which the asymptotic solution lies within T1(1) but below B∞,s,2, suggesting the possibility that there are additional unresolved bands with even finer structure. Other than these six points, trajectories emanating from all MICs lying near, but outside of, the secondary band have B = B∞,s,1, with −174πθ ≤ −154π or 141πθ ≤ 163π, ranges similar to those found in Sec. 4.1 with larger increments of ηi and θi over a larger part of the MIC space.

Comparing results for δ = 10−8 (Tables S2(a) and S2(b) available in the Supplemental Materials) and δ = 10−10 (Tables S3(a) and S3(b) available in the Supplemental Materials), we see that asymptotic states corresponding to “isolated points” in Region IV are invariant to integration tolerance. To verify that the band structure described above is insensitive to integration tolerance, we computed B and θ for 201 MICs, for 4.372 ≤ ηi ≤ 4.392 and θi = 0.4π integrated with δ = 10−8 and 10−10 (Table S5 available in the Supplemental Materials). The locations of band boundaries are essentially identical, as are values of B and θ within the bands. Outside of the bands, where transient chaos leads to asymptotic states with B = B∞,s,1, the values of θ vary slightly with integration tolerance.

In Region V, for MICs with ηi > 4.5 lying on or near the extension of the left branch of the primary band shown in Fig. 11(a), Figs. 13(a)13(c) show B distributions in rectangular neighborhoods centered at (ηi, θi) = (4.5530, 0.341π), (4.5960, 0.331π), and (4.6582, 0.318π). As one moves upward and leftward in Region IV along the primary band (from Figs. 13(a) to 13(b) to 13(c)) toward Region V, the relatively wide, well-defined internal structure of the primary band becomes increasingly complex, suggesting transition from fractality to riddling.

Fig. 13
For (α, σ, λ) = (1, 0.01, 0), asymptotic amplitude in the neighborhood of (a) (ηi, θi) = (4.5530, 0.341π), (b) (ηi, θi) = (4.5960, 0.331π), and (c) (ηi, θi) = (4.6582, 0.318π). B∞ = B∞,s,1, orange; B∞ = B∞,s,2, gray; A1(1) < B∞ < B∞,s,2, blue; and B∞,s,2 < B∞ < A2(1), black.
Fig. 13
For (α, σ, λ) = (1, 0.01, 0), asymptotic amplitude in the neighborhood of (a) (ηi, θi) = (4.5530, 0.341π), (b) (ηi, θi) = (4.5960, 0.331π), and (c) (ηi, θi) = (4.6582, 0.318π). B∞ = B∞,s,1, orange; B∞ = B∞,s,2, gray; A1(1) < B∞ < B∞,s,2, blue; and B∞,s,2 < B∞ < A2(1), black.
Close modal

Analogous to the asymptotic amplitudes B in T1(1) for isolated MICs in Region IV, MICs in Region V with A3(1) ≤ ηiA4(1) and θi departing from 0 and π can lead to trajectories with A3(1) ≤ BA4(1) (see Table S2(a) available in the Supplemental Materials). A key difference for these Region V MICs, in T2(1), is that sampling the MIC space with the same increment in θi and an increment in ηi comparable with that used in T1(1) reveals no additional MICs (i.e., not close to θi = 0 or π) for which A3(1) ≤ BA4(1). If such MICs exist, in bands even thinner than their T1(1) analogues, none were found.

5.2 Scales of True and Amplitude-Only Basins of Attraction in Region V.

To quantitatively understand the structure of basins leading to special-amplitude solutions with B = B∞,s,1 or B∞,s,2, we follow the procedure described earlier [5] to approximate scales of the true basins of attraction (denoted by s(B,nπ)) and amplitude-only basins (denoted by sB), in which (B, ) and B, respectively, are locally insensitive to initial-condition perturbations. Note, however, that the values of s(B,nπ) and sB do not directly establish fractality or riddling in the MIC space, and that small values can only suggest riddling. The distinction between fractality and riddling is more clearly established by an uncertainty exponent [19], computed following our earlier procedure [5] presented in Sec. 5.3.

In Region V, the scales s(B,nπ) and sB for which (B, θ) or just B, respectively, are insensitive to initial-condition perturbations, are calculated by an approach similar to that used earlier [5]. For 4 ≤ K ≤ 11, we compute (B, θ) at a nominal MIC (ηi,nom, θi,nom) and four nearby MICs (ηi,nom, θi,nom ± 10K) and (ηi,nom ± 10K, θi,nom). We begin with K = 12, for which we compute (B, θ) at these five and 12 other MICs, (ηi,nom ± 10−12, θi,nom + 10−12), (ηi,nom ± 10−12, θi,nom − 10−12), (ηi,nom + 10−12, θi,nom ± 5 × 10−13), (ηi,nom − 10−12, θi,nom ± 5 × 10−13), (ηi,nom ± 5 × 10−13, θi,nom + 10−12), and (ηi,nom ± 5 × 10−13, θi,nom − 10−12). We then decrease K by unity, each time computing (B, θ) at four new points until not all solutions are identical. The scale s(B,nπ) corresponds to the largest among nine values of ɛp = 10K for which (ηi,nom, θi,nom) and all 16 + 4(12 − K) perturbed MICs lead to the same (B, θ). Similarly, sB is the largest ɛp for which B is identical at the same MICs.

Figure 14(a) shows distributions of B and sB (the scale of a neighborhood in MIC space in which B is insensitive), with values of the latter generally decreasing with increasing ηi, suggesting that the amplitude-only basins of attraction become more fractal, consistent with Figs. 13(a)13(c). In Fig. 14(a), all MICs for which sB1012 and ηi ≥ 5.48 are seen to have B = B∞,s,2. This suggests that for ηi ≥ 5.48, all MICs lying in connected portions of an amplitude-only basin lead to a T1(1) time-harmonic special solution. For ηi ≥ 5.72, no point with sB1012 is found, suggesting that this portion of the MIC space is riddled.

Fig. 14
For (α, σ, λ) = (1, 0.01, 0), distributions of (a) sB∞ (scale of regions in which B∞ is identical), and (b) s(B∞,nπ) (scale of regions in which (B∞, nπ) is identical) computed with the relative and absolute integration tolerances δ = 10−8. sB∞ and s(B∞,nπ): ≥10−4, unfilled (white); 10−5 and 10−6, gray; 10−7 and 10−8, blue; 10−9 and 10−10, green; 10−11 and 10−12, red; and <10−12, black. B∞ = B∞,s,1, squares; B∞ = B∞,s,2, diamonds; B∞ lying within T1(1) with B∞ ≠ B∞,s,2, crosses, for which B∞ is a continuous variable so that sB∞ and s(B∞,nπ) are not defined.
Fig. 14
For (α, σ, λ) = (1, 0.01, 0), distributions of (a) sB∞ (scale of regions in which B∞ is identical), and (b) s(B∞,nπ) (scale of regions in which (B∞, nπ) is identical) computed with the relative and absolute integration tolerances δ = 10−8. sB∞ and s(B∞,nπ): ≥10−4, unfilled (white); 10−5 and 10−6, gray; 10−7 and 10−8, blue; 10−9 and 10−10, green; 10−11 and 10−12, red; and <10−12, black. B∞ = B∞,s,1, squares; B∞ = B∞,s,2, diamonds; B∞ lying within T1(1) with B∞ ≠ B∞,s,2, crosses, for which B∞ is a continuous variable so that sB∞ and s(B∞,nπ) are not defined.
Close modal

Figure 14(b) shows the distributions of B and s(B,nπ) for 4.4 ≤ ηi ≤ 6.0. In this range, all MICs leading to a ground-state time-harmonic special solution have s(B,nπ)<1012, suggesting that the true basins of attraction for MICs leading to solutions with this special amplitude are riddled. This is consistent with the riddling associated with θ sensitivity identified in Region III [5], in which all trajectories have asymptotic rectilinear amplitude B∞,s,1. As ηi increases, s(B,nπ) generally decreases for points leading to B∞,s,2, indicating that the true basins either remain fractal but become smaller, or transition from fractal to riddled. Again, no MIC gives s(B,nπ)1012 for ηi ≥ 5.72, suggesting that this portion of the MIC space is riddled.

The general trends of sB and s(B,nπ) are the same when trajectories are integrated with δ = 10−10 (compare Figs. 14(a) and S7(a), and Figs. 14(b) and S7(b) available in the Supplemental Materials), indicating that the observed behavior is a property of the differential equation system and is not due to numerical artifacts.

5.3 Characterization of Riddling and Fractality.

In Region III, B assumes a single nonzero value (B∞,s,1) over a range of MICs, while θ is sensitive to initial conditions [5]. This is also true in parts of Regions IV and V. Elsewhere in Region V, both B and θ can be sensitive to initial conditions. The scales of the true and amplitude-only basins of attraction generally decrease and become exceedingly small as ηi increases, suggesting that the behavior for large ηi is either fractal or riddled. However, as mentioned in Sec. 5.2, basin structure cannot be established directly by values of s(B,nπ) (or sB), but can be characterized by the related uncertainty exponent [19], which we compute for the true basins (denoted by atrue) and amplitude-only basins (aB), closely following our previous procedure [5]. In each square neighborhood of MICs centered about (ηi,cen, θi,cen), we determine atrue and aB from 400 randomly selected nominal MICs, each with four neighboring perturbed MICs for each of several values of the perturbation magnitude ɛp. For each ɛp and each B (or combination of B and θ), we compute gB (or gtrue) as the fraction of the points at which there is “amplitude sensitivity” (or “solution sensitivity”). The slope of a plot of the logarithm of gB (or gtrue) versus the logarithm of ɛp provides aB (or atrue), whose value identifies fractal behavior (aB or atrue not close to zero) or riddling behavior (aB or atrue close to zero) [19].

Neighborhood 1. Fractal amplitude-only basins of attraction and riddled true basins of attraction. For a square neighborhood of edge length 2 × 10−5 centered at (ηi,cen, θi,cen) = (4.7, 0.5π), we compute (B, ) for 400 randomly selected MICs. For 13 values of 10−12ɛp ≤ 10−6, the distribution of B for all 21,200 (=400 × (13 × 4 + 1)) MICs is shown in Fig. 15(a), where a series of parallel bands giving rise to identical B is evident. From the 400 nominal MICs, we excluded 15 for which B is neither B∞,s,1 nor B∞,s,2. We calculated gB and gtrue by using the 385 nominal MICs leading to either B∞,s,1 (of which there are 180) or B∞,s,2 (of which there are 205) to generate 20,405 (=385 × (13 × 4 + 1)) perturbed MICs. The results give aB=0.248, showing that the amplitude-only basins for B∞,s,1 and B∞,s,2 are fractal (see Fig. 15(b)).

Fig. 15
For (α, σ, λ) = (1, 0.01, 0) and 400 MICs in a square neighborhood of edge length 2 × 10−5 centered at (ηi,cen, θi,cen) = (4.7, 0.5π), (a) distribution of B∞, (b) fraction gB∞, (c) fraction gtrue, and (d) fraction gtrue, computed considering only the 205 MICs attracted to B∞,s,2. In (a), B∞ = B∞,s,1, orange; B∞ = B∞,s,2, gray; and other B∞ lying in T1(1) and B∞ ≠ B∞,s,2, blue. In (b–d), calculated gB∞ and gtrue, circles; linear least-squares fit, solid line.
Fig. 15
For (α, σ, λ) = (1, 0.01, 0) and 400 MICs in a square neighborhood of edge length 2 × 10−5 centered at (ηi,cen, θi,cen) = (4.7, 0.5π), (a) distribution of B∞, (b) fraction gB∞, (c) fraction gtrue, and (d) fraction gtrue, computed considering only the 205 MICs attracted to B∞,s,2. In (a), B∞ = B∞,s,1, orange; B∞ = B∞,s,2, gray; and other B∞ lying in T1(1) and B∞ ≠ B∞,s,2, blue. In (b–d), calculated gB∞ and gtrue, circles; linear least-squares fit, solid line.
Close modal

In this neighborhood of fractal amplitude-only basins, we characterized the true basins. Figure 15(c) shows the dependence of gtrue on ɛp for 10−12ɛp ≤ 10−6. For 10−9ɛp ≤ 10−6, log gtrue increases linearly with increasing log ɛp, having slope atrue = 0.105. For 10−12ɛp ≤ 10−10.5, log gtrue is nearly constant (gtrue ≈ 0.4675), indicating riddling for sufficiently small ɛp. This disjointedness of gtrue indicates coexistence of fractality and riddling of the true basins in this neighborhood.

To establish this, we consider separately the true basins of attraction for B∞,s,1 and those for B∞,s,2. Among the 400 randomly selected MICs, examination of the 180 for which B = B∞,s,1 shows that each is sensitive to initial conditions (i.e., gtrue = 1 for ɛp ≤ 10−6). Thus, in the neighborhood of the central MIC (ηi, θi) = (4.7, 0.5π), all randomly selected MICs leading to B∞,s,1 lie in riddled true basins, consistent with the result in Fig. 15(c) that the limiting value gtrue ≈ 0.4675 is the fraction of MICs leading to a ground-state time-harmonic special solution (180/385 = 0.4675…). Figure 15(d) shows log gtrue calculated using the 205 random MICs for which B = B∞,s,2. Linear dependence of log gtrue on log ɛp establishes the fractal nature of all true basins giving B∞,s,2 and further verifies that fractal and riddled true basins are intertwined within the neighborhood, as reported previously in another context [20].

Neighborhood 2. Portions of MIC space with riddled amplitude-only and true basins of attraction. For a square neighborhood of edge length 2 × 10−9 centered at (ηi,cen, θi,cen) = (5.7, 0.85π), we extracted atrue = 0 and aB=0.0048 for 10−13ɛp ≤ 10−10 (Figs. S8(a) and S8(b) available in the Supplemental Materials), showing that the true and amplitude-only basins of attraction are riddled [19] in this neighborhood. From the distribution of B (Fig. S8(c) available in the Supplemental Materials), it is apparent that there is no systemic variation of B in this MIC neighborhood.

6 Results for (α, σ, λ) = (0.1, 0.1, 0)

For (α, σ, λ) = (0.1, 0.1, 0), Fig. 16(a) shows the B distribution for 2451 MICs (43 θi and 57 ηi) in Region III which, as shown in Fig. 5(b), begins near ηi = 0.4638 and extends to at least ηi = 15, well beyond A4(0.1). The distribution is qualitatively similar to that for smaller ηi in Region III (0.4638… = A0(0.1) ≤ ηiA1(0.1) = 3.7617…) [5]. Tables S6(a) and S6(b) available in the Supplemental Materials show B and θ, respectively, for 3804 additional MICs (A1(0.1) ≤ ηi ≤ 15 and 0 < θi < π). Unlike the (α, σ, λ) = (1, 0.01, 0) case, there is no large set of MICs leading to a single nonzero asymptotic amplitude. In Fig. 16(a), only three MICs, (ηi, θi) = (3.8, 0.99π), (3.8, 0.999π), and (5.4, 0.475π), identified by pink dots, lead to B values lying within T1(0.1). The other 2448 MICs in Fig. 16(a) have 0 ≤ B < 0.161 (including 849 with B = 0), and thus dissipate at least 99.82% of the initial energy. These results clearly show that for (α, σ, λ) = (0.1, 0.1, 0), larger initial energies will have no effect on the asymptotic rectilinear amplitude, except in exceedingly narrow parts of the MIC space.

Fig. 16
For (α, σ, λ) = (0.1, 0.1, 0), distributions of (a) B∞ for 2451 MICs (43 θi and 57 ηi); (b) P0, defined as fraction of 43 θi for which the MIC leads to B∞ = 0 at each of 57 ηi; and (c) B∞ for 10,201 MICs (101 θi and 101 ηi) within |ηi − 6.6| ≤ 10−5 and |θi − 0.5π| ≤ 10−5. In (a and c), B∞ = 0, black; 0 < B∞ < A0(0.1), false-color scale; A1(0.1) < B∞ < A2(0.1), pink (three points in Fig. 16(a), and 14 points in Fig. 16(c)).
Fig. 16
For (α, σ, λ) = (0.1, 0.1, 0), distributions of (a) B∞ for 2451 MICs (43 θi and 57 ηi); (b) P0, defined as fraction of 43 θi for which the MIC leads to B∞ = 0 at each of 57 ηi; and (c) B∞ for 10,201 MICs (101 θi and 101 ηi) within |ηi − 6.6| ≤ 10−5 and |θi − 0.5π| ≤ 10−5. In (a and c), B∞ = 0, black; 0 < B∞ < A0(0.1), false-color scale; A1(0.1) < B∞ < A2(0.1), pink (three points in Fig. 16(a), and 14 points in Fig. 16(c)).
Close modal

The observed sensitivity in asymptotic amplitude is related to the transient chaos in trajectories, resulting in a riddled zero-energy amplitude-only basin. (For (α, σ, λ) = (0.1, 0.1, 0), the true and amplitude-only basins of attraction are not well defined for B ≠ 0, as B can assume any one of an uncountable number of values and no nonzero B is the asymptotic amplitude for a large number of MICs.)

For each of 57 uniformly incremented ηi in the range 3.8 ≤ ηi ≤ 15, Fig. 16(b) gives P0, the fraction of the 43 θi values shown in Fig. 16(a) leading to a zero-energy solution. This fraction does not systematically depend on ηi, continuing the behavior found for ηi ranging from about 1.7 to A1(0.1) = 3.7617… (see Fig. 14(c) of Ref. [5]). In the neighborhood (6.6 − 10−5ηi ≤ 6.6 + 10−5, 0.5π − 10−5θi ≤ 0.5π + 10−5), Fig. 16(c) shows the B distribution for 10,201 MICs (101 uniformly incremented ηi and θi). In this neighborhood, there exist several apparently isolated points (pink) leading to B values lying within T1(0.1), showing that even though the initial coupling strength is strong (with θi departing strongly from an integer multiple of π), there are MICs for which only a small fraction of the initial energy is dissipated. In addition to the MICs giving rise to nonzero B, the complicated distribution of MICs leading to zero-energy solutions (black) in Fig. 16(c) is reminiscent of the riddled behavior for (α, σ, λ) = (1, 0.01, 0) (Sec. 5.3), due to sensitivity of B attributable to passage through transient chaos. (It is possible that these apparently isolated MICs lie on a fractal band, as shown in Figs. 16(a) and 16(b) of Ref. [5], and in Sec. 5.1 for (α, σ, λ) = (1, 0.01, 0).) To characterize the zero-energy amplitude-only basins, we examine an additional 400 randomly selected nominal MICs leading to zero-energy solutions (none from among the 10,201 points considered above). Calculation of aB=0 closely follows our previous procedure [5], with each random MIC that leads to a zero-energy solution being perturbed in each of four directions, (ηi ± ɛp, θi) and (ηi, θi ± ɛp), for nine perturbation magnitudes 10−8ɛp ≤ 10−6. The uncertainty exponent of that basin is aB=0=1.025×103, indicating riddling [19].

Near θi = 0 and π, there exist ηi (3.7617… = A1(0.1) ≤ ηi ≤ 3.812) for which B depends continuously on the MIC (Table S6(a) available in the Supplemental Materials) and the asymptotic state is rapidly approached with no chaotic transient, with θ being the integer multiple of π nearest to θi. This continuous variation of B is similar to that found in Regions IIA and IIB for (α, σ, λ) = (0.1, 0.1, 0) and (1, 0.01, 0) [4], but unlike the (α, σ, λ) = (1, 0.01, 0) approach of B to a single value as ηi increases, for (α, σ, λ) = (0.1, 0.1, 0) there are no special oscillation amplitudes to which wide ranges of MICs are led.

Figures 17(a) and 17(b) show the ηi-dependence of θ for a wide range of MICs (162 values of ηi for 0.48 ≤ ηi ≤ 24 and 43 values of θi for 10−3πθi ≤ 0.999π, with ηi increments of 0.04 for 0.48 ≤ ηi ≤ 4, 0.2 for 4 ≤ ηi ≤ 15 and 0.5 for 15 ≤ ηi ≤ 24). Each point is colored according to its B value. For 2.2 ≤ ηi ≤ 12.2, the θ values for semi-trivial and zero-energy solutions lie in two nearly symmetric bands of roughly equal extent, with 0 ≤ |θ| ≤ 83π. As ηi increases beyond 13.4, the ranges of θ increasingly and symmetrically depart from θ = 0. Beyond ηi = 16.5, the two ranges no longer change, with 64π ≤ |θ| ≤ 411π. Comparing Figs. 17(a) and 17(b), we see that departure of the θ bands from θ = 0 at small ηi and then again near ηi = 13.4, in both cases followed by an ηi range in which band width is independent of ηi, is similar. Whether a third departure occurs for larger ηi is unclear.

Fig. 17
For (α, σ, λ) = (0.1, 0.1, 0), distribution of θ∞ over 0 < θi < π for (a) 0.4 ≤ ηi ≤ 4.0 and (b) 4 ≤ ηi ≤ 24. B∞ = 0, black; 0 < B∞ < A0(0.1), false-color scale; A1(0.1) < B∞ < A2(0.1), pink dots, larger for clarity.
Fig. 17
For (α, σ, λ) = (0.1, 0.1, 0), distribution of θ∞ over 0 < θi < π for (a) 0.4 ≤ ηi ≤ 4.0 and (b) 4 ≤ ηi ≤ 24. B∞ = 0, black; 0 < B∞ < A0(0.1), false-color scale; A1(0.1) < B∞ < A2(0.1), pink dots, larger for clarity.
Close modal

7 Damping of The Rectilinear Motion of The Primary Mass

With direct rectilinear damping (λ > 0), all asymptotic states have zero energy (i.e., B = 0). For ηiA1(α), we focus on characterizing energy dissipation using the “settling time” required to dissipate 99% of the initial energy, denoted by τ0.01 [4,5]. This is a useful measure because dissipation can occur (simultaneously or during different stages of the decay process) by means of both rotational and direct rectilinear damping, in either case with significant nonlinear effects, thus limiting use of a single-exponential decay model. Here, we discuss the dependence of τ0.01 on MICs and the relationship to the λ = 0 results discussed above. We also show results for the fraction of the energy dissipation attributable to rotational damping, β.

7.1 General Dependence of Energy Dissipation for λ>0.

For (α, σ, λ) = (0.1, 0.1, λ) with 3.5 ≤ ηi ≤ 15 and θi = 0.5π (for which initial “leverage” is greatest), Fig. 18(a) shows the dependence of τ0.01 on ηi, for λ = 10−5, 10−4, 10−3, 3 × 10−3, and 10−2, the same values considered previously [5]. For each λ, τ0.01 generally increases as ηi increases, over the entire range. For 10−5 < λ ≤ 10−2, the mean value of 0.01/i (averaged over the ηi range) decreases as λ increases. Comparison with Fig. 18(b) of Ref. [5] shows that the relatively weak and generally monotonic dependence of τ0.01 on ηi and λ in this range of ηi continues the behavior found in Region III for 1.21 ≤ ηi ≤ 3.76, in contrast to more complex behavior found for smaller ηi in that region. “Dips” in τ0.01 as a function of ηi are associated with initial-condition sensitivity of trajectories, as discussed for smaller ηi [5]. This sensitivity means that there are values of ηi for which increased direct rectilinear damping counterintuitively increases τ0.01, e.g., τ0.01(ηi = 7.25, λ = 10−4) > τ0.01(ηi = 7.25, λ = 10−5). Similar sensitivity can be expected with respect to θi.

Fig. 18
Variation of τ0.01 with ηi for (a) (α, σ) = (0.1, 0.1), and (b) (α, σ) = (1, 0.01). λ = 10−5, orange; λ = 10−4, green; λ = 10−3, blue; λ = 3 × 10−3, pink; λ = 10−2, black
Fig. 18
Variation of τ0.01 with ηi for (a) (α, σ) = (0.1, 0.1), and (b) (α, σ) = (1, 0.01). λ = 10−5, orange; λ = 10−4, green; λ = 10−3, blue; λ = 3 × 10−3, pink; λ = 10−2, black
Close modal

For (α, σ, λ) = (1, 0.01, λ) with θi = 0.5π, the dependence of τ0.01 on ηi and λ is quite different. Figure 18(b) shows that τ0.01 depends weakly on ηi for λ = 10−3, 3 × 10−3, and 10−2, making clear that the stronger ηi variation for all five λ values at smaller ηi (see Fig. 17(b) of Ref. [5]) does not extend to Regions IV and V. (The results shown in Fig. 18(b) are displayed as a plot of λτ0.01 versus ηi in Fig. S9(b) available in the Supplemental Materials, for more direct comparison to Fig. 17(b) of Ref. [5].) The dips in τ0.01 (Fig. 18(b)), over 90% for λ = 10−4 and almost 99% for λ = 10−5, are attributable to initial-condition sensitivity that carries over from the λ = 0 case. This is illustrated for λ = 10−4 in Figs. 19(a)19(d), where apparent randomness of these dips persists down to increments between consecutive values of ηi far smaller than the value (0.25) used in Fig. 18(b). This is directly traceable to initial-condition sensitivity exhibited by trajectories for nearby MICs (Figs. S10(a)S10(d) available in the Supplemental Materials). Implications of this sensitivity for design are discussed in Sec. 8. The dual-value nature of the fine-scale sensitivity apparent in Figs. 19(a)19(d), with all values of τ0.01 being near 4.1 × 104 or 1.5 × 104, strongly suggests association with the initial-condition sensitivity of B in the λ = 0 case, which leads to two dominant values of B, namely, B∞,s,1 and B∞,s,2.

Fig. 19
For (α, σ, λ) = (1, 0.01, 10−4) with θi = 0.5π, variation of τ0.01 with ηi over (a) 5.9 ≤ ηi ≤ 6.1, (b) 5.99 ≤ ηi ≤ 6.01, (c) 5.999 ≤ ηi ≤ 6.001, and (d) 6 − 10−4 ≤ ηi ≤ 6 + 10−4
Fig. 19
For (α, σ, λ) = (1, 0.01, 10−4) with θi = 0.5π, variation of τ0.01 with ηi over (a) 5.9 ≤ ηi ≤ 6.1, (b) 5.99 ≤ ηi ≤ 6.01, (c) 5.999 ≤ ηi ≤ 6.001, and (d) 6 − 10−4 ≤ ηi ≤ 6 + 10−4
Close modal

For (α, σ, λ) = (0.1, 0.1, λ) with θi = 0.5π, the fraction of dissipation attributable to rotational damping, β, decreases nearly monotonically as ηi and λ increase (Fig. S11(a) available in the Supplemental Materials). Local dips in β as a function of ηi again result from initial-condition sensitivity. As for τ0.01, there are combinations of ηi and λ for which β depends nonmonotonically on λ. For (α, σ, λ) = (1, 0.01, λ), the more complex dependence of β on ηi and λ (Fig. S11(b) available in the Supplemental Materials) reflects more complex dependence of B on ηi for (α, σ, λ) = (1, 0.01, 0) compared with (α, σ, λ) = (0.1, 0.1, 0). (For (α, σ, λ) = (0.1, 0.1, 0) and A2(0.1) < ηi ≤ 15, recall from Sec. 6 that 2448 of 2451 MICs lead to trajectories dissipating at least 99.82% of the initial energy, whereas for (α, σ, 0) = (1, 0.01, 0) essentially all trajectories lead to asymptotic solutions with amplitudes lying in one of three ranges of orbital stability, with almost all in two of those ranges.)

7.2 Initial-Condition Sensitivity for λ>0.

To further explore initial-condition sensitivity of the settling time τ0.01, and the relationship to initial-condition sensitivity for λ = 0, we examine small neighborhoods in MIC space, as we did for λ = 0 in Secs. 5.2 and 5.3.

As shown in Sec. 2 for λ = 0, the duration of transient chaos for trajectories with similar ηi is longer for those with asymptotic amplitude B∞,s,1 than for those with B = B∞,s,2. For λ > 0, the need to dissipate all initial energy leads to significant variation in settling time. To relate the λ = 0 MIC dependence of asymptotic amplitude to the λ > 0 MIC dependence of settling time, we consider (α, σ, λ) = (1, 0.01, 0) and extract B for 651 uniformly incremented MICs (at 31 ηi and 21 θi) in the rectangular neighborhood 4.43 − 5 × 10−3ηi ≤ 4.43 + 10−2, 0.475π − 5 × 10−3θi ≤ 0.475π + 5 × 10−3). We then consider six nonzero λ ranging from 10−5 to 7 × 10−4, and for each λ compute the corresponding distributions of τ0.01 (Figs. 20(a)20(f)) and β (Figs. 21(a)21(f)), as well as the maximum variation of λτ0.01 in the neighborhood, denoted by Δ(λτ0.01) = λ(τ0.01,maxτ0.01,min), and the corresponding Δβ = βmaxβmin.

Fig. 20
For 4.43 − 5 × 10−3 ≤ ηi ≤ 4.43 + 10−2 and 0.475π − 5 × 10−3 ≤ θi ≤ 0.475π + 5 × 10−3 with (α, σ) = (1, 0.01), distributions of λτ0.01 for (a) λ = 10−5, (b) λ = 10−4, (c) λ = 3 × 10−4, (d) λ = 5 × 10−4, (e) λ = 6 × 10−4, and (f) λ = 7 × 10−4; (g) distribution of B∞ for λ = 0, In (a–f), 1.9 ≤ λτ0.01 < 2.1, blue; 2.1 ≤ λτ0.01 < 2.3, cyan; 2.3 ≤ λτ0.01 < 2.5, green; 2.5 ≤ λτ0.01 < 2.7, yellow; 2.7 ≤ λτ0.01 ≤ 2.8, gray; and 4.4 ≤ λτ0.01 ≤ 4.6, red. No MIC gives 2.8 < λτ0.01 < 4.4. In (g), B∞ = B∞,s,1, pink; A1(1) ≤ B∞ ≤ A2(1), black.
Fig. 20
For 4.43 − 5 × 10−3 ≤ ηi ≤ 4.43 + 10−2 and 0.475π − 5 × 10−3 ≤ θi ≤ 0.475π + 5 × 10−3 with (α, σ) = (1, 0.01), distributions of λτ0.01 for (a) λ = 10−5, (b) λ = 10−4, (c) λ = 3 × 10−4, (d) λ = 5 × 10−4, (e) λ = 6 × 10−4, and (f) λ = 7 × 10−4; (g) distribution of B∞ for λ = 0, In (a–f), 1.9 ≤ λτ0.01 < 2.1, blue; 2.1 ≤ λτ0.01 < 2.3, cyan; 2.3 ≤ λτ0.01 < 2.5, green; 2.5 ≤ λτ0.01 < 2.7, yellow; 2.7 ≤ λτ0.01 ≤ 2.8, gray; and 4.4 ≤ λτ0.01 ≤ 4.6, red. No MIC gives 2.8 < λτ0.01 < 4.4. In (g), B∞ = B∞,s,1, pink; A1(1) ≤ B∞ ≤ A2(1), black.
Close modal
Fig. 21
For 4.43 − 5 × 10−3 ≤ ηi ≤ 4.43 + 10−2 and 0.475π − 5 × 10−3 ≤ θi ≤ 0.475π + 5 × 10−3 with (α, σ) = (1, 0.01), distributions of β for (a) λ = 10−5, (b) λ = 10−4, (c) λ = 3 × 10−4, (d) λ = 5 × 10−4, (e) λ = 6 × 10−4, and (f) λ = 7 × 10−4. 0 ≤ β ≤ 0.1, blue; 0.5 ≤ β < 0.6, green; 0.6 ≤ β < 0.7, yellow; 0.7 ≤ β < 0.8, gray; 0.8 ≤ β < 0.9, brown; 0.9 ≤ β ≤ 1, red. No MIC gives 0.1 < β < 0.5.
Fig. 21
For 4.43 − 5 × 10−3 ≤ ηi ≤ 4.43 + 10−2 and 0.475π − 5 × 10−3 ≤ θi ≤ 0.475π + 5 × 10−3 with (α, σ) = (1, 0.01), distributions of β for (a) λ = 10−5, (b) λ = 10−4, (c) λ = 3 × 10−4, (d) λ = 5 × 10−4, (e) λ = 6 × 10−4, and (f) λ = 7 × 10−4. 0 ≤ β ≤ 0.1, blue; 0.5 ≤ β < 0.6, green; 0.6 ≤ β < 0.7, yellow; 0.7 ≤ β < 0.8, gray; 0.8 ≤ β < 0.9, brown; 0.9 ≤ β ≤ 1, red. No MIC gives 0.1 < β < 0.5.
Close modal

Figures 20(a)20(f) and 21(a)21(f) show distributions of λτ0.01 and β, respectively, for the same 651 MICs. Except for Fig. 20(f), each subfigure displays a band structure similar to that shown for B in Fig. 20(g) when λ = 0, where a primary band, with A1(1) < B < A2(1), is apparently accompanied by a series of unresolved secondary bands, indicating a fractal distribution of B. For the same set of MICs, we compute the distributions of λτ0.01 and β for λ = 10−5, whose fractal structures (Figs. 20(a) and 21(a)) are in both cases qualitatively similar to that for B, with Δ(λτ0.01) = 2.63 and Δβ = 0.908 over the range of MICs. As λ increases to 6 × 10−4, the MIC band narrows and shifts slightly upward for both λτ0.01 and β (Figs. 20(b)20(e) and 21(b)21(e)), and the variations diminish (Table 3). For λ = 7 × 10−4, there is no obvious variation of λτ0.01 (Fig. 20(f)), while the banding for β is still evident (Fig. 21(f)). This is consistent with the much more rapid decrease of Δ(λτ0.01) between λ = 6 × 10−4 and 7 × 10−4 compared with the decrease in Δβ (Table 3), and indicates that as λ approaches 7 × 10−4, direct rectilinear damping is sufficient to suppress initial-condition sensitivity of λτ0.01 and β caused by transient chaos in this neighborhood.

Table 3

For (α, σ) = (1, 0.01), variation of λτ0.01 and β, in which Δ(λτ0.01) = λ(τ0.01,maxτ0.01,min) and Δβ = βmaxβmin, calculated for 651 MICs lying within the rectangular neighborhood (4.43 − 5 × 10−3ηi ≤ 4.43 + 10−2, 0.475π − 5 × 10−3θi ≤ 0.475π + 5 × 10−3), and from 441 MICs lying within the neighborhood (6 − 10−8ηi ≤ 6 + 10−8, 0.5π − 10−8θi ≤ 0.5π + 10−8)

(ηi,cen, θi,cen) = (4.43, 0.475π)(ηi,cen, θi,cen) = (6, 0.5π)
λ(λτ0.01)Δβλ(λτ0.01)Δβ
10−52.6290.90810−52.6510.510
10−42.5350.87610−42.5950.513
3 × 10−42.3570.8083 × 10−42.4340.486
5 × 10−42.2100.7555 × 10−42.2850.461
6 × 10−42.1430.7307 × 10−42.0950.394
7 × 10−40.2190.1519 × 10−40.2830.126
(ηi,cen, θi,cen) = (4.43, 0.475π)(ηi,cen, θi,cen) = (6, 0.5π)
λ(λτ0.01)Δβλ(λτ0.01)Δβ
10−52.6290.90810−52.6510.510
10−42.5350.87610−42.5950.513
3 × 10−42.3570.8083 × 10−42.4340.486
5 × 10−42.2100.7555 × 10−42.2850.461
6 × 10−42.1430.7307 × 10−42.0950.394
7 × 10−40.2190.1519 × 10−40.2830.126

The relationship between MIC sensitivity of B for λ = 0 and MIC sensitivity of τ0.01 and β for λ > 0 is also observed in the riddled MIC neighborhood (6 − 10−8ηi ≤ 6 + 10−8, 0.5π − 10−8θi ≤ 0.5π + 10−8). For 10−5λ ≤ 10−3, Figs. 22(a)22(f) and 23(a)23(f) show the distributions of τ0.01 and β, respectively. In this neighborhood, for λ ≥ 9 × 10−4, the initial-condition sensitivity of λτ0.01 and β is greatly diminished (Table 3). For (α, σ, λ) = (1, 0.01, 0), Fig. 22(g) shows a riddled distribution of B within the neighborhood containing 441 MICs (21 uniformly incremented values each of ηi and θi). These results clearly show that initial-condition sensitivity of the λ = 0 response provides good guidance to the sensitivity of energy dissipation under weak direct rectilinear damping. As λ increases beyond a critical value, riddled behavior of τ0.01 and β is suppressed, which explains why in Fig. 18(b), there is no significant variation in τ0.01 for λ ≥ 10−3. As shown in Figs. 18(a) and 18(b), direct rectilinear damping reduces initial-condition sensitivity of τ0.01 and β but does not eliminate it (see Fig. S12 available in the Supplemental Materials for λ = 10−3).

Fig. 22
For 6 − 10−8 ≤ ηi ≤ 6 + 10−8 and 0.5π − 10−8 ≤ θi ≤ 0.5π + 10−8 with (α, σ) = (1, 0.01), distribution of λτ0.01 for (a) λ = 10−5, (b) λ = 10−4, (c) λ = 3 × 10−4, (d) λ = 5 × 10−4, (e) λ = 7 × 10−4, and (f) λ = 9 × 10−4; (g) distribution of B∞ for λ = 0. In (a–f), 1.3 ≤ λτ0.01 < 1.6, blue; 1.6 ≤ λτ0.01 < 1.9, cyan; 1.9 ≤ λτ0.01 < 2.2, green; 2.2 ≤ λτ0.01 < 2.4, yellow; 2.4 ≤ λτ0.01 ≤ 2.6, gray; 3.9 ≤ λτ0.01 ≤ 4.3, red. No MIC gives 2.6 < λτ0.01 < 3.9. In (g), B∞ = B∞,s,1, pink dots; B∞ = B∞,s,2, black dots; and A1(1) < B∞ < B∞,s,2, open circles.
Fig. 22
For 6 − 10−8 ≤ ηi ≤ 6 + 10−8 and 0.5π − 10−8 ≤ θi ≤ 0.5π + 10−8 with (α, σ) = (1, 0.01), distribution of λτ0.01 for (a) λ = 10−5, (b) λ = 10−4, (c) λ = 3 × 10−4, (d) λ = 5 × 10−4, (e) λ = 7 × 10−4, and (f) λ = 9 × 10−4; (g) distribution of B∞ for λ = 0. In (a–f), 1.3 ≤ λτ0.01 < 1.6, blue; 1.6 ≤ λτ0.01 < 1.9, cyan; 1.9 ≤ λτ0.01 < 2.2, green; 2.2 ≤ λτ0.01 < 2.4, yellow; 2.4 ≤ λτ0.01 ≤ 2.6, gray; 3.9 ≤ λτ0.01 ≤ 4.3, red. No MIC gives 2.6 < λτ0.01 < 3.9. In (g), B∞ = B∞,s,1, pink dots; B∞ = B∞,s,2, black dots; and A1(1) < B∞ < B∞,s,2, open circles.
Close modal
Fig. 23
For 6 − 10−8 ≤ ηi ≤ 6 + 10−8 and 0.5π − 10−8 ≤ θi ≤ 0.5π + 10−8 with (α, σ) = (1, 0.01), distribution of β for (a) λ = 10−5, (b) λ = 10−4, (c) λ = 3 × 10−4, (d) λ = 5 × 10−4, (e) λ = 7 × 10−4, and (f) λ = 9 × 10−4. 0.3 ≤ β < 0.4, blue; 0.4 ≤ β < 0.5, black; 0.5 ≤ β < 0.6, green; 0.6 ≤ β < 0.7, yellow; 0.7 ≤ β < 0.8, gray; 0.8 ≤ β < 0.9, brown; 0.9 ≤ β ≤ 1, red. No MIC gives 0 ≤ β < 0.3.
Fig. 23
For 6 − 10−8 ≤ ηi ≤ 6 + 10−8 and 0.5π − 10−8 ≤ θi ≤ 0.5π + 10−8 with (α, σ) = (1, 0.01), distribution of β for (a) λ = 10−5, (b) λ = 10−4, (c) λ = 3 × 10−4, (d) λ = 5 × 10−4, (e) λ = 7 × 10−4, and (f) λ = 9 × 10−4. 0.3 ≤ β < 0.4, blue; 0.4 ≤ β < 0.5, black; 0.5 ≤ β < 0.6, green; 0.6 ≤ β < 0.7, yellow; 0.7 ≤ β < 0.8, gray; 0.8 ≤ β < 0.9, brown; 0.9 ≤ β ≤ 1, red. No MIC gives 0 ≤ β < 0.3.
Close modal

For (α, σ, 0) = (0.1, 0.1, 0), the initial-condition sensitivity of B to ηi is much weaker and so no strong sensitivity of τ0.01 and β is found. The general dependence of τ0.01 and β on ηi is qualitatively similar to that for A0(0.1) ≤ ηiA1(0.1) [5].

8 Discussion

8.1 General Considerations.

For one combination of damping coefficient and coupling coefficient (α = 1, σ = 0.01) and no direct rectilinear damping, a wide range of motionless initial conditions gives rise to three sets of asymptotically nonrotating “time-harmonic special solutions,” each with amplitude in one of the three lowest-lying ranges of orbitally stable solutions. Initial-condition sensitivity associated with transient chaos leads to fractality and riddling in the initial-condition space with respect to both asymptotic amplitude of the rectilinear oscillation and final angular orientation. For α = 1 and σ = 0.01, no motionless initial condition with initial rectilinear amplitude above the lowest value at which instability is possible leads to a zero-energy solution, with the primary and NES masses at rest.

For α = 1 and σ = 0.01, the results presented in Sec. 4 strongly suggest that the amplitude-only basin of attraction of asymptotic solutions with the special amplitude B∞,s,3 = 11.2020156… in tongue T2(1) does not extend beyond the small regions shown in Fig. 6(a). On the other hand, trajectories emanating from a broad class of initial conditions (including initial rectilinear displacements only slightly larger than the special amplitudes B∞,s,1 = 1.1712734… or B∞,s,2 = 4.4056717…) lead to solutions with B∞,s,1 and B∞,s,2. That is simply not the case for B∞,s,3.

For the other combination (α = σ = 0.1), zero-energy solutions are found for a wide range of motionless initial conditions. The amplitude-only basin of attraction (i.e., the set of motionless initial conditions for which the asymptotic rectilinear amplitude is zero regardless of final angular orientation) is riddled. This behavior is qualitatively similar to that found at smaller initial rectilinear displacements [5].

For α = 1 and σ = 0.01, the results in Sec. 4.2 clearly establish that except in exceedingly small parts of the MIC space, asymptotic solutions with rectilinear amplitude greater than A2(1) = 4.40642… will not be found regardless of how large the initial energy is. Similarly, results in Sec. 6 show that for α = σ = 0.1, asymptotic solutions with amplitude greater than A2(0.1) = 3.7961… will be found only in very limited parts of the MIC space, regardless of initial energy. Temptation to generalize to other combinations of α and σ is tempered by the fact that the distributions of asymptotic amplitudes below A2(α) are so different for the two combinations investigated.

Finally, initial-condition sensitivity for the case where there is no direct damping of rectilinear motion (λ = 0) provides good guidance to understand the response for λ > 0 cases where such damping is accounted for, including cases where fractality or riddling of the amplitude-only basins of attraction in the λ = 0 case correspond to fractality or riddling of the settling time for λ > 0.

8.2 Relationship to Applications.

Sensitivity to initial conditions can pose a significant challenge to use of a rotational NES in applications, as discussed previously [5]. One can of course attempt to avoid combinations of the parameters (α, σ, and λ) for which performance (e.g., the settling time τ0.01) is significantly sensitive over the expected range of initial conditions. Alternatively, there are various probabilistic design approaches to dealing with the sensitivity [5], including developing bounds for best and worst cases, using the methods of uncertainty quantification [21], and using information about the probability distribution of initial energies to compute probability distributions for response measures such as settling time. For both (α, σ) combinations, our results point to probabilistic interpretation of the final state [5], and prediction of the probabilities that the asymptotic harmonic motion has an amplitude B equal to (a) zero; (b) one of the time-harmonic special solutions; or (c) a value in one of the first three ranges of orbital stability, but not equal to that of the time-harmonic special solution lying in that range. More generally, for any initial condition, one can specify the size of a neighborhood, and then compute the probabilities that the asymptotic rectilinear amplitude or angular orientation lie in a given range (or their joint probability). When trajectories depend sensitively on initial conditions, this approach can serve as the basis for probabilistic design.

From the standpoint of settling time, Fig. 18(a) clearly shows that the degree of initial-condition sensitivity of τ0.01 is quite large for (α, σ) = (0.1, 0.1) at small values of the rectilinear damping parameter λ. For (α, σ) = (0.1, 0.1) and the two smallest values of λ considered (10−4 and 10−5), Fig. 18(a) shows that although τ0.01 varies by approximately a factor of five over the indicated range of ηi, the variation is nearly monotonic (and approximately linear with ηi). Moreover, the local variation in τ0.01 attributable to initial-condition sensitivity is quite small (less than 20%), especially in comparison with the variations for (α, σ) = (1, 0.01) of well over 90% for small λ shown in Fig. 18(b). These marked differences point to the importance of understanding the degree of sensitivity for any set of parameters used in design.

For (α, σ, λ) = (0.1, 0.1, 0) and no direct rectilinear damping, Fig. 16(a) and the accompanying discussion show that for 2451 initial conditions over a wide range, all of the initial energy was dissipated for 849 of them, and that for all but three of the others, at least 99.82% almost all (at least 99.82%) was dissipated. From an application standpoint, this is a much more favorable result than might be inferred for (α, σ, λ) = (0.1, 0.1, 0) results at lower initial energy reported in Ref. [1], where two of the six trajectories dissipated more than 98% of the initial energy, and the others dissipated approximately 42%, 24%, 15%, and 0%. (No trajectory shown in Ref. [1] has an initial condition for which all initial energy is dissipated [4]. Note also that the results reported in Ref. [2] for nonzero rotational damping at higher initial energy were computed at a single initial rectilinear displacement, and include no values of asymptotic rectilinear amplitude.) On the other hand, three of the 2451 initial conditions lead to asymptotic solutions having significant rectilinear amplitudes, illustrating the importance of thoroughly exploring the initial-condition space in order to identify “outliers.”

Finally, in applications, the initial conditions cannot always be expected to be motionless. For (α, σ, λ) = (0.1, 0.1, 0) with the same (ηi, θi) considered in Fig. 16(a) and vi = Ωi = 0.1, Fig. 24 shows the distribution of B, with 820 of the 2451 initial conditions leading to zero-energy solutions, and the remainder having B < 0.1473. Thus, for each of the initial conditions considered, over 99.95% of the initial energy (see Eq. (5) of Ref. [4]) is dissipated. Other than the fact that none of the initial conditions gives rise to a solution with B lying in T1(0.1) (as opposed to three such solutions for the 2451 MICs considered in Fig. 16(a)) the number of zero-energy solutions and the fraction of energy dissipation are qualitatively similar to the results for motionless initial conditions shown in Fig. 16(a) (849 zero-energy solutions, and the remainder dissipating at least 99.82% of the initial energy). This, along with similar results reported previously [4,5], supports the hypothesis that our sensitivity results are not limited to the motionless subspace of initial conditions.

Fig. 24
For (α, σ, λ) = (0.1, 0.1, 0) with vi = Ωi = 0.1, distribution of B∞ for the 2451 (ηi, θi) considered in Fig. 16(a), with 820 of them leading to B∞ = 0. B∞ = 0, black; 0 < B∞ < A0(0.1), false-color scale
Fig. 24
For (α, σ, λ) = (0.1, 0.1, 0) with vi = Ωi = 0.1, distribution of B∞ for the 2451 (ηi, θi) considered in Fig. 16(a), with 820 of them leading to B∞ = 0. B∞ = 0, black; 0 < B∞ < A0(0.1), false-color scale
Close modal

9 Conclusions

For a rotational nonlinear energy sink inertially coupled to a linear oscillator, we have examined the part of the motionless projection of the initial-condition space (i.e., with the initial rectilinear and angular velocities zero) in which the initial rectilinear displacement (ηi) exceeds the second threshold amplitude above which purely rectilinear time-harmonic motion is unstable. Absent direct rectilinear damping (λ = 0), for one combination of the dimensionless coupling parameter (α = 1) and dimensionless rotational damping parameter (σ = 0.01), no motionless initial condition leads to a zero-energy solution (in which all initial energy is dissipated). For this range of ηi, almost all initial conditions lead to asymptotically nonrotating semi-trivial solutions for which the rectilinear amplitude is either the smallest “special” amplitude (B∞,s,1) or lies in the first tongue in which nonrotating rectilinearly harmonic solutions are orbitally stable. The exceptions are in very small parts of the motionless initial-condition space where ηi lies in or just above the extremely narrow second or third tongues in which semi-trivial solutions are orbitally stable, and the initial angular position of the NES mass departs only minutely from an integer multiple of π. Most initial conditions leading to solutions with asymptotic amplitudes in the first tongue have the second-smallest special amplitude (B∞,s,2). The basins of attraction of solutions with special asymptotic amplitudes B∞,s,1 or B∞,s,2 are fractal or riddled in the motionless initial-condition space. For initial rectilinear displacements beyond those considered here, our results strongly suggest that asymptotic solutions with other amplitudes (i.e., lying in the second or third tongues of orbital stability) are possible only for exceedingly small sets of the motionless initial conditions.

In stark contrast are results for the other combination of parameters (α = σ = 0.1), where the dimensionless rotational damping parameter is 90% smaller and the dimensionless coupling parameter is higher by tenfold. For this case, many initial conditions lead to zero-energy solutions, for which the amplitude-only basin of attraction (i.e., the set of motionless initial conditions for which the asymptotic amplitude is zero, irrespective of asymptotic angular orientation) is riddled. Almost all motionless initial conditions are attracted to either zero-energy solutions or to solutions for which at least 99.82% of the initial energy is dissipated. The exceptions are some with initial rectilinear displacements in or just above the first tongue of orbital stability with departure of the initial angular orientation from an integer multiple of π being exceedingly small, and some apparently isolated initial conditions for which the initial angular orientation is not close to an integer multiple of π. No special-amplitude solutions (i.e., solutions with a common nonzero amplitude, to which many initial conditions are led) are found.

For both combinations of the parameters, the results clearly establish that asymptotic solutions with rectilinear amplitude greater than the upper bound of the second tongue occur only in exceedingly limited parts of the motionless condition space, regardless of how large the initial energy is.

Finally, when one accounts for direct rectilinear damping (λ > 0), the asymptotic rectilinear amplitude is necessarily zero, and the time required to dissipate 99% of the initial energy (τ0.01) can depend complexly and nonmonotonically on the initial conditions and rectilinear damping parameter, with the distribution of asymptotic rectilinear amplitudes for λ = 0 providing good guidance as to the distribution in the motionless initial-condition space of both τ0.01 and the fraction of energy dissipation attributable to rotational damping.

Acknowledgment

The authors gratefully acknowledge support from National Science Foundation (NSF) Grant CMMI-1363231.

Conflict of Interest

There are no conflicts of interest.

Data Availability Statement

The authors attest that all data for this study are included in the paper.

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