Dynamic vibration and quasi-static deformation will occur simultaneously for flexible space structures subjected to sudden thermal loads. In this paper, the integrated controller based on modified positive position feedback (PPF) compensator is proposed as an innovative controller for active deformation reduction in flexible space trusses. The controller uses the concept of positive acceleration feedback combined with integral position feedback to provide effective vibration suppression of multiple modes and compensator of quasi-static deformation. To solve the problem of placement optimization for both sensors and actuators, the discrete glowworm swarm optimization (GSO) algorithm based on genic binary coding is suggested. A cantilevered truss is taken as an example for numerically evaluating the performance of the controller for thermally induced deformation control. Numerical results demonstrate that the discrete GSO algorithm is feasible in solving the combinatorial optimization problem. And the proposed controller is significantly effective in controlling both steady-state deformation and transient vibration.
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August 2016
Research-Article
Integrated Control of Thermally Induced Vibration and Quasi-Static Deformation of Space Truss
Jie Wang,
Jie Wang
College of Aerospace Science and Engineering,
National University of Defense Technology,
No. 47 Yanwachi Street,
Changsha 410073, China
e-mail: wangjie@nudt.edu.cn
National University of Defense Technology,
No. 47 Yanwachi Street,
Changsha 410073, China
e-mail: wangjie@nudt.edu.cn
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Dongxu Li,
Dongxu Li
College of Aerospace Science and Engineering,
National University of Defense Technology,
No. 47 Yanwachi Street,
Changsha 410073, China
e-mail: dongxuli@nudt.edu.cn
National University of Defense Technology,
No. 47 Yanwachi Street,
Changsha 410073, China
e-mail: dongxuli@nudt.edu.cn
Search for other works by this author on:
Jianping Jiang
Jianping Jiang
College of Aerospace Science and Engineering,
National University of Defense Technology,
No. 47 Yanwachi Street,
Changsha 410073, China
e-mail: jianpingjiang@nudt.edu.cn
National University of Defense Technology,
No. 47 Yanwachi Street,
Changsha 410073, China
e-mail: jianpingjiang@nudt.edu.cn
Search for other works by this author on:
Jie Wang
College of Aerospace Science and Engineering,
National University of Defense Technology,
No. 47 Yanwachi Street,
Changsha 410073, China
e-mail: wangjie@nudt.edu.cn
National University of Defense Technology,
No. 47 Yanwachi Street,
Changsha 410073, China
e-mail: wangjie@nudt.edu.cn
Dongxu Li
College of Aerospace Science and Engineering,
National University of Defense Technology,
No. 47 Yanwachi Street,
Changsha 410073, China
e-mail: dongxuli@nudt.edu.cn
National University of Defense Technology,
No. 47 Yanwachi Street,
Changsha 410073, China
e-mail: dongxuli@nudt.edu.cn
Jianping Jiang
College of Aerospace Science and Engineering,
National University of Defense Technology,
No. 47 Yanwachi Street,
Changsha 410073, China
e-mail: jianpingjiang@nudt.edu.cn
National University of Defense Technology,
No. 47 Yanwachi Street,
Changsha 410073, China
e-mail: jianpingjiang@nudt.edu.cn
1Corresponding author.
Contributed by the Dynamic Systems Division of ASME for publication in the JOURNAL OF DYNAMIC SYSTEMS, MEASUREMENT, AND CONTROL. Manuscript received June 27, 2015; final manuscript received March 31, 2016; published online May 25, 2016. Assoc. Editor: Ming Xin.
J. Dyn. Sys., Meas., Control. Aug 2016, 138(8): 081003 (8 pages)
Published Online: May 25, 2016
Article history
Received:
June 27, 2015
Revised:
March 31, 2016
Citation
Wang, J., Li, D., and Jiang, J. (May 25, 2016). "Integrated Control of Thermally Induced Vibration and Quasi-Static Deformation of Space Truss." ASME. J. Dyn. Sys., Meas., Control. August 2016; 138(8): 081003. https://doi.org/10.1115/1.4033407
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