Reentry Attitude Control of Reusable Launch Vehicle Based on Event-Triggered Sliding Mode Control

In order to deal with unknown external disturbances in the reentry phase and save communication resource. In this paper, an event-triggered scheme based on sliding mode control is designed for the attitude regulation of a class of Reusable Launch Vehicle in reentry phase subject to unknown external...

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Vydané v:2021 IEEE International Conference on Electronic Technology, Communication and Information (ICETCI) s. 306 - 312
Hlavní autori: Wen, Baoyu, Huang, Jiangshuai, Tan, Yaoyao, Gao, Tingting
Médium: Konferenčný príspevok..
Jazyk:English
Vydavateľské údaje: IEEE 27.08.2021
Predmet:
Attitude control
Backstepping
Conferences
Event-triggered algorithm
Measurement errors
Regulation
Reusable Launch Vehicle
Sliding mode control
Stability analysis
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Shrnutí:In order to deal with unknown external disturbances in the reentry phase and save communication resource. In this paper, an event-triggered scheme based on sliding mode control is designed for the attitude regulation of a class of Reusable Launch Vehicle in reentry phase subject to unknown external disturbances. A sliding control mode based on event-triggered is designed and based on which the attitude control design of Reusable Launch Vehicle in reentry phase is proposed using backstepping technique. The stability analysis is given via Lyapunov function technique. Finally, the effectiveness of developed control scheme is validated through simulations.
DOI:10.1109/ICETCI53161.2021.9563541