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 |
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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. |
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| 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 |
| Author_xml | – sequence: 1 givenname: Hongyan surname: Zhang fullname: Zhang, Hongyan email: zhanghongyan@bit.edu.cn organization: School of Aerospace Engineering, Beijing Institute of Technology,Beijing,China – sequence: 2 givenname: Shiyao surname: Lin fullname: Lin, Shiyao email: kent_linsy@126.com organization: Chinese Research and Development, Academy of Equipment,Beijing,China – sequence: 3 givenname: Yuchan surname: Wang fullname: Wang, Yuchan email: wycc@bit.edu.cn organization: School of Aerospace Engineering, Beijing Institute of Technology,Beijing,China – sequence: 4 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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| 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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