Disturbance Observer-Based Fixed-Time Attitude Autopilot for Guided Projectile

In this paper, a robust attitude autopilot for spinning glide guided projectile is presented. Combing with the idea of trajectory linearization control (TLC), a TLC based fixed-time converged integral sliding mode control scheme is present. Moreover, to estimate and compensate total uncertainties, a...

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Vydané v:	Proceedings of ... IEEE International Conference on Unmanned Systems (Online) s. 58 - 63
Hlavní autori:	Zhang, Hongyan, Lin, Shiyao, Wang, Yuchan, Wang, Wei
Médium:	Konferenčný príspevok..
Jazyk:	English
Vydavateľské údaje:	IEEE 13.10.2023
Predmet:	Attitude control Autopilot extended state observer fixed-time stable theory integral sliding mode Observers Projectiles spinning glide guided projectiles Stability analysis Trajectory trajectory linearization control Uncertainty
ISSN:	2771-7372
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Popis
Shrnutí:	In this paper, a robust attitude autopilot for spinning glide guided projectile is presented. Combing with the idea of trajectory linearization control (TLC), a TLC based fixed-time converged integral sliding mode control scheme is present. Moreover, to estimate and compensate total uncertainties, a reduced-order extended state observer is developed. The stability of closed-loop system is verified via Lyapunov method. Finally, numerical simulation is carried out to demonstrate the efficiency of proposed attitude autopilot.
ISSN:	2771-7372
DOI:	10.1109/ICUS58632.2023.10318391