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Observer-based attitude control of spacecraft under actuator dead zone and misalignment faults

Author

Listed:
  • Javaid, Umair
  • Zhen, Ziyang
  • Shahid, Sami
  • Ibrahim, Dauda Sh
  • Ijaz, Salman

Abstract

The paper discusses the effect of non-smooth dead-zone (NDZ), and input actuator misalignment (AMA) during spacecraft attitude tracking maneuver in presence of parametric uncertainties and external perturbations. Initially, the input AMA and NDZ models are formulated to transform spacecraft attitude model dynamics. Subsequently, a new second order disturbance observer (SODO) is devised to get the total disturbance. The observer is developed considering system perturbations as extended states, with an additional term Introduced to improve the observer performance. Finally, a distinctive integral sliding mode control (ISMC) law is developed and integrated with the proposed SODO to perform spacecraft attitude control operations. Comparative simulations are conducted on the spacecraft attitude control model with input AMA, NDZ, system parametric uncertainties and external disturbances to show the effectiveness of the proposed control structure.

Suggested Citation

  • Javaid, Umair & Zhen, Ziyang & Shahid, Sami & Ibrahim, Dauda Sh & Ijaz, Salman, 2024. "Observer-based attitude control of spacecraft under actuator dead zone and misalignment faults," Applied Mathematics and Computation, Elsevier, vol. 465(C).
    • Handle: RePEc:eee:apmaco:v:465:y:2024:i:c:s0096300323005751
    DOI: 10.1016/j.amc.2023.128406
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    References listed on IDEAS

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    1. Xu, Xiaofeng & Chen, Mou & Li, Tao & Wu, Qingxian, 2021. "Composite fault tolerant attitude control for flexible satellite system under disturbance and input delay," Applied Mathematics and Computation, Elsevier, vol. 409(C).
    2. Vimal Kumar, S. & Raja, R. & Marshal Anthoni, S. & Cao, Jinde & Tu, Zhengwen, 2018. "Robust finite-time non-fragile sampled-data control for T-S fuzzy flexible spacecraft model with stochastic actuator faults," Applied Mathematics and Computation, Elsevier, vol. 321(C), pages 483-497.
    3. Ijaz, Salman & Fuyang, Chen & Hamayun, Mirza Tariq & Anwaar, Haris, 2021. "Adaptive integral-sliding-mode control strategy for maneuvering control of F16 aircraft subject to aerodynamic uncertainty," Applied Mathematics and Computation, Elsevier, vol. 402(C).
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