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标题:Finite-time spacecraft attitude control under input magnitude and rate saturation
时间:2021-04-08 15:57:51
DOI:10.1007/s11071-019-05388-6
大小:2409 kb
页数:18 PAGES
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目录:
  • Finite-time spacecraft attitude control under input magnitude and rate saturation
    • Abstract
    • 1 Introduction
    • 2 Preliminaries
      • 2.1 Notations, definitions, and lemmas
      • 2.2 Attitude kinematics and dynamics of rigid spacecraft
    • 3 Main results
      • 3.1 New input magnitude and rate model
      • 3.2 Design of finite-time attitude-stabilizing control scheme using angular velocity measurements
      • 3.3 Design of velocity-free finite-time attitude-stabilizing control scheme
    • 4 Simulation results
    • 5 Conclusions
    • Acknowledgements
    • Appendices
      • Proof of Theorem 1
      • Proof of Proposition 1
      • Proof of Theorem 3
      • Proof of Theorem 4
    • References

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