Abstract

Many modern-day applications involve transport of objects suspended through cables such as in overhead cranes or landing of rovers on the Martian surface. Any undesired oscillation of the payload has the potential risk of instability, and the problem of damping such oscillation and stabilizing the payload at the desired length is the control objective of this article. The system is modeled as a variable length pendulum (VLP), which comprises a payload suspended via a string wrapped around a pulley. The length of the pendulum is varied using clockwise/counterclockwise rotation of the pulley through torque applied by a motor. For a known payload mass, a nonlinear control design is first presented that guarantees asymptotic stability of the desired equilibrium with limited state measurements. The design is then modified for it to handle significant uncertainty in payload mass. The effectiveness of both designs is validated in simulations.

References

1.
Anderle
,
M.
,
Michiels
,
W.
,
Čelikovskỳ
,
S.
, and
Vyhlídal
,
T.
,
2019
, “
Damping a Pendulum’s Swing by String Length Adjustment-Design and Comparison of Various Control Methods
,”
American Control Conference
,
Philadelphia, PA
,
July
, pp.
4399
4405
.
2.
Čelikovskỳ
,
S.
,
Anderle
,
M.
, and
Vyhlídal
,
T.
,
2020
, “
Underactuated Pendulum Damping by Its Length Adjustment and Passive Output Selection
,”
2020 European Control Conference
,
St. Petersburg, Russia
,
May 12–15
, pp.
100
105
.
3.
Guerrero-Sánchez
,
M. E.
,
Mercado-Ravell
,
D. A.
,
Lozano
,
R.
, and
García-Beltrán
,
C. D.
,
2017
, “
Swing-Attenuation for a Quadrotor Transporting a Cable-Suspended Payload
,”
ISA Trans.
,
68
, pp.
433
449
.
4.
Homolka
,
P.
,
Hromčík
,
M.
, and
Vyhlídal
,
T.
,
2017
, “
Input Shaping Solutions for Drones With Suspended Load: First Results
,”
International Conference on Process Control
,
Strbske Pleso, Slovakia
,
June 6–9
, pp.
30
35
.
5.
Hyla
,
P.
,
2012
, “
The Crane Control Systems: A Survey
,”
International Conference on Methods & Models in Automation & Robotics
,
Miedzyzdroje, Poland
,
Aug. 27–30
, IEEE, pp.
505
509
.
6.
Kant
,
N.
,
2020
,
Exploiting Impulsive Inputs for Stabilization of Underactuated Robotic Systems: Theory and Experiments
,
Michigan State University
,
East Lansing, MI
.
7.
Khalil
,
H. K.
,
2002
,
Nonlinear Systems
,
Prentice Hall
,
Upper Saddle River, NJ
.
8.
Kuře
,
M.
,
Bušek
,
J.
,
Vyhlídal
,
T.
, and
Niculescu
,
S.-I.
,
2021
, “
Algorithms for Cable-Suspended Payload Sway Damping by Vertical Motion of the Pivot Base
,”
Mech. Syst. Signal. Process.
,
149
, p.
107131
.
9.
Masoud
,
Z. N.
,
Nayfeh
,
A. H.
, and
Al-Mousa
,
A.
,
2003
, “
Delayed Position-Feedback Controller for the Reduction of Payload Pendulations of Rotary Cranes
,”
J. Vib. Control
,
9
(
1–2
), pp.
257
277
.
10.
Tuan
,
L.A.
,
Moon
,
S.C.
,
Lee
,
W.G
, and
Lee
,
S.G
,
2013
, “
Adaptive Sliding Mode Control of Overhead Cranes With Varying Cable Length
,”
J. Mech. Sci. Tech.
,
27
(
3
), pp.
885
893
.
11.
Longhao
,
Q.
,
Silas
,
G.
, and
Liu
,
H. H-T
,
2020
, “
Guidance and Control Law Design for a Slung Payload in Autonomous Landing: A Drone Delivery Case Study
,”
IEEE/ASME Trans. Mech.
,
25
(
4
), pp.
1773
1782
.
12.
Helicopter Tree Sawing In The MD 500
,
2015
, https://www.youtube.com/watch?v=Pla06PO6Odk
13.
Stilling
,
D. S. D.
, and
Szyszkowski,
,
W.
,
2002
, “
Controlling Angular Oscillations Through Mass Reconfiguration: A Variable Length Pendulum Case
,”
Int. J. Non-Linear Mech.
,
37
(
1
), pp.
89
99
.
14.
Vaughan
,
J.
,
Kim
,
D.
, and
Singhose
,
W.
,
2010
, “
Control of Tower Cranes With Double-Pendulum Payload Dynamics
,”
IEEE Trans. Control Syst. Tech.
,
18
(
6
), pp.
1345
1358
.
15.
Vyhlídal
,
T.
,
Anderle
,
M.
,
Bušek
,
J.
, and
Niculescu
,
S.-I.
,
2017
, “
Time-Delay Algorithms for Damping Oscillations of Suspended Payload by Adjusting the Cable Length
,”
IEEE/ASME Trans. Mech.
,
22
(
5
), pp.
2319
2329
.
16.
Way
,
D. W.
,
Powell
,
R. W.
,
Chen
,
A.
,
Steltzner
,
A. D.
,
Martin
,
A. M. S.
,
Burkhart
,
P. D.
, and
Mendeck
,
G. F.
,
2007
, “
Mars Science Laboratory: Entry, Descent, and Landing System Performance
,”
Aerospace Conference
,
Big Sky, MT
,
Mar. 3–10
, pp.
1
19
.
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