AI Chat Paper
Note: Please note that the following content is generated by AMiner AI. SciOpen does not take any responsibility related to this content.
{{lang === 'zh_CN' ? '文章概述' : 'Summary'}}
{{lang === 'en_US' ? '中' : 'Eng'}}
Chat more with AI
Powered by AMiner. Clicking this button will take you away from SciOpen.
Home Tsinghua Science and Technology Article
PDF (69.7 MB)
Cite
EndNote(RIS) BibTeX
Collect
Submit Manuscript AI Chat Paper
Show Outline
Outline
Show full outline
Hide outline
Outline
Show full outline
Hide outline
Open Access

Adaptive Prescribed Performance Control for Flexible Spacecraft with Input Saturation and Actuator Misalignment

Department of Automation, Tsinghua University, Beijing 100084, China.
Department of Strategic Missile and Underwater Weapon, Naval Submarine Academy, Qingdao 266071, China.
Show Author Information

Abstract

In this paper, a flexible spacecraft attitude control scheme that guarantees vibration suppression and prescribed performance on transient-state behavior is proposed. Here, parametric uncertainty, external disturbance, unmeasured elastic vibration, actuator saturation, and even configuration misalignment are considered. To guarantee prescribed performance bounds on the transient- and steady-state control errors, a performance constrained control law is formulated with an error transformed function. An elastic modal observer is employed to estimate the unmeasured flexible modal variables, and a command filter is adopted to avoid the tedious analytical computations of time derivatives of virtual control inherent in the control design. Subsequently, a novel auxiliary system is developed to compensate the adverse effects of the actuator saturation constraints, and a compensation term is integrated into the control law to tackle the configuration misalignment. A comparative simulation study is carried out to illustrate the effectiveness and advantages of the proposed approach.

Keywords

flexible spacecraftmodal observervibration suppressionprescribed performanceinput saturationactuator misalignment

References

[1]
Guo Y., Zhou C. F., Yu Z., and Chen Q. W., Study on attitude control for move-to-rest manoeuvre of flexible spacecraft, International Journal of Modelling, Identification and Control, vol. 19, no. 1, pp. 23-31, 2013.
Crossref Google Scholar
[2]
Zhong C. X., Lai A. F., Guo Y., and Chen Q. W., On attitude maneuver control of flexible spacecraft without angular velocity sensors, in Proc. 2013 IEEE/SICE Int. Symp. System Integration, Kobe, Japan, 2013, pp. 318-323.
Crossref
[3]
Zhong C. X., Chen Z. Y., and Guo Y., Attitude control for flexible spacecraft with disturbance rejection, IEEE Transactions on Aerospace and Electronic Systems, vol. 53, no. 1, pp. 101-110, 2017.
Crossref Google Scholar
[4]
Zhong C. X., Guo Y., Yu Z., Wang L., and Chen Q. W., Finite-time attitude control for flexible spacecraft with unknown bounded disturbance, Transactions of the Institute of Measurement and Control, vol. 38, no. 2, pp. 240-249, 2016.
Crossref Google Scholar
[5]
Di Gennaro S., Output attitude tracking for flexible spacecraft, Automatica, vol. 38, no. 10, pp. 1719-1726, 2002.
Crossref Google Scholar
[6]
Di Gennaro S., Output stabilization of flexible spacecraft with active vibration suppression, IEEE Transactions on Aerospace and Electronic Systems, vol. 39, no. 3, pp. 747-759, 2003.
Crossref Google Scholar
[7]
Di Gennaro S., Passive attitude control of flexible spacecraft from quaternion measurements, Journal of Optimization Theory and Applications, vol. 116, no. 1, pp. 41-60, 2003.
Crossref Google Scholar
[8]
Di Gennaro S., Tracking control using attitude measurements for flexible spacecraft in presence of disturbances, in Proc. 43rd IEEE Conf. Decision and Control, Nassau, Bahamas, 2004, pp. 2123-2128.
Crossref
[9]
Wang N., Wu H. N., and Guo L., Coupling-observer-based nonlinear control for flexible air-breathing hypersonic vehicles, Nonlinear Dynamics, vol. 78, no. 3, pp. 2141-2159, 2014.
Crossref Google Scholar
[10]
Boškovic J. D., Li S. M., and Mehra R. K., Robust adaptive variable structure control of spacecraft under control input saturation, Journal of Guidance, Control, and Dynamics, vol. 24, no. 1, pp. 14-22, 2001.
Crossref Google Scholar
[11]
Boškovic J. D., Li S. M., and Mehra R. K., Robust tracking control design for spacecraft under control input saturation, Journal of Guidance, Control, and Dynamics, vol. 27, no. 4, pp. 627-633, 2004.
Crossref Google Scholar
[12]
Zou A. M., de Ruiter A. H. J., and Kumar K. D., Finite-time attitude tracking control for rigid spacecraft with control input constraints, IET Control Theory and Applications, vol. 11, no. 7, pp. 931-940, 2017.
Crossref Google Scholar
[13]
Li B., Hu Q. L., and Ma G. F., Extended state observer based robust attitude control of spacecraft with input saturation, Aerospace Science and Technology, vol. 50, pp. 173-182, 2016.
Crossref Google Scholar
[14]
Ma J. J., Li P., Geng L., and Zheng Z. Q., Adaptive finite-time attitude tracking control of an uncertain spacecraft with input saturation, in Proc. 2015 IEEE Conf. Control Applications, Sydney, Australia, 2015, pp. 930-935.
[15]
Hu Q. L., Li B., and Qi J. T., Disturbance observer based finite-time attitude control for rigid spacecraft under input saturation, Aerospace Science and Technology, vol. 39, pp. 13-21, 2014.
Crossref Google Scholar
[16]
Hu Q. L., Robust adaptive sliding mode attitude maneuvering and vibration damping of three-axis-stabilized flexible spacecraft with actuator saturation limits, Nonlinear Dynamics, vol. 55, no. 4, pp. 301-321, 2009.
Crossref Google Scholar
[17]
Hu Q. L. and Xiao B., Robust adaptive backstepping attitude stabilization and vibration reduction of flexible spacecraft subject to actuator saturation, Journal of Vibration and Control, vol. 17, no. 11, pp. 1657-1671, 2011.
Crossref Google Scholar
[18]
Bechlioulis C. P. and Rovithakis G. A., Adaptive control with guaranteed transient and steady state tracking error bounds for strict feedback systems, Automatica, vol. 45, no. 2, pp. 532-538, 2009.
Crossref Google Scholar
[19]
Wu Z. H., Lu J. C., Shi J. P., Zhou Q., and Qu X. B., Tracking error constrained robust adaptive neural prescribed performance control for flexible hypersonic flight vehicle, International Journal of Advanced Robotic Systems, vol. 14, no. 1, pp.1-16, 2017.
Crossref Google Scholar
[20]
Bu X. W., Wu X. Y., Zhu F. J., Huang J. Q., Ma Z., and Zhang R., Novel prescribed performance neural control of a flexible air-breathing hypersonic vehicle with unknown initial errors, ISA Transactions, vol. 59, pp. 149-159, 2015.
Crossref Google Scholar
[21]
Bu X. W., Wu X. Y., Huang J. Q., and Wei D. Z., A guaranteed transient performance-based adaptive neural control scheme with low-complexity computation for flexible air-breathing hypersonic vehicles, Nonlinear Dynamics, vol. 84, no. 4, pp. 2175-2194, 2016.
Crossref Google Scholar
[22]
Hu Q. L., Shao X. D., and Guo L., Adaptive fault-tolerant attitude tracking control of spacecraft with prescribed performance, IEEE/ASME Transactions on Mechatronics, vol. 23, no. 1, pp. 331-341, 2018.
Crossref Google Scholar
[23]
Polycarpou M. M., Stable adaptive neural control scheme for nonlinear systems, IEEE Transactions on Automatic Control, vol. 41, no. 3, pp. 447-451, 1996.
Crossref Google Scholar
[24]
Polycarpou M. M. and Ioannou P. A., A robust adaptive nonlinear control design, Automatica, vol. 32, no. 3, pp. 423-427, 1996.
Crossref Google Scholar
[25]
Farrell J. A., Polycarpou M., Sharma M., and Dong W. J., Command filtered backstepping, IEEE Transactions on Automatic Control, vol. 54, no. 6, pp. 1391-1395, 2009.
Crossref Google Scholar
[26]
Xia K. W. and Huo W., Robust adaptive backstepping neural networks control for spacecraft rendezvous and docking with input saturation, ISA Transactions, vol. 62, pp. 249-257, 2016.
Crossref Google Scholar
[27]
Jiao X. H. and Zhang L. Y., Adaptive output feedback control of attitude maneuver and vibration suppression for flexible spacecraft, (in Chinese), Electric Machines and Control, vol. 15, no. 7, pp. 94-100, 2011.
Google Scholar
Tsinghua Science and Technology
Volume 24 Issue 6,
December 2019
Pages 694-705
DOI: 10.26599/TST.2018.9010094
Cite this article:
Tao J, Zhang T, Nie Y. Adaptive Prescribed Performance Control for Flexible Spacecraft with Input Saturation and Actuator Misalignment. Tsinghua Science and Technology, 2019, 24(6): 694-705. https://doi.org/10.26599/TST.2018.9010094

727

Views

28

Downloads

6

Crossref

N/A

Web of Science

9

Scopus

3

CSCD

Altmetrics
Received: 11 February 2018
Revised: 18 April 2018
Accepted: 19 April 2018
Published: 05 December 2019
© The author(s) 2019
Return