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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Veröffentlicht in:Proceedings of ... IEEE International Conference on Unmanned Systems (Online) S. 58 - 63
Hauptverfasser: Zhang, Hongyan, Lin, Shiyao, Wang, Yuchan, Wang, Wei
Format: Tagungsbericht
Sprache:Englisch
Veröffentlicht: IEEE 13.10.2023
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ISSN:2771-7372
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Abstract 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.
AbstractList 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.
Author Zhang, Hongyan
Wang, Yuchan
Wang, Wei
Lin, Shiyao
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  givenname: Shiyao
  surname: Lin
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  givenname: Yuchan
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  organization: School of Aerospace Engineering, Beijing Institute of Technology,Beijing,China
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  givenname: Wei
  surname: Wang
  fullname: Wang, Wei
  email: wangweiyh@bit.edu.cn
  organization: School of Aerospace Engineering, Beijing Institute of Technology,Beijing,China
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Snippet In this paper, a robust attitude autopilot for spinning glide guided projectile is presented. Combing with the idea of trajectory linearization control (TLC),...
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StartPage 58
SubjectTerms 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
Title Disturbance Observer-Based Fixed-Time Attitude Autopilot for Guided Projectile
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