Journal
IEEE TRANSACTIONS ON SYSTEMS MAN CYBERNETICS-SYSTEMS
Volume 52, Issue 10, Pages 6674-6678Publisher
IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC
DOI: 10.1109/TSMC.2022.3145508
Keywords
Attitude control; Manifolds; Heuristic algorithms; Upper bound; Vehicle dynamics; Robustness; Aerodynamics; Adaptive multivariable control; attitude control of reusable launch vehicle (RLV); prescribed performance
Funding
- National Natural Science Foundation of China [62022060, 61773278, 61873340, 61903349, 62073234, 62003236]
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In this paper, a novel adaptive multivariable control algorithm is proposed for reusable launch vehicle (RLV). The algorithm is simple and easy to implement, and utilizes Lyapunov-based technique to guarantee error confinement within prescribed regions.
A novel adaptive multivariable control algorithm is proposed for reusable launch vehicle (RLV) subject to bounded but unknown disturbances. In the proposed algorithm, a time-varying nonoverestimated adaptive gain is designed based on the prescribed performance function. The proposed method is very simple and easy implementation, and the Lyapunov-based technique is utilized to guarantee that the reentry attitude tracking errors are confined in some prescribed regions independent of the upper bound of the disturbances. Finally, the efficiency of the developed algorithm is illustrated by simulation results.
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