Practical Finite-Time Attitude Reorientation Control for Rigid Spacecraft With Forbidden Pointing Constraints and Physical Limitations

This article investigates the spacecraft attitude reorientation problem with forbidden pointing constraints and physical limitations. Relying on kinematics of the spacecraft, a nominal virtual angular velocity is first designed to guarantee that the spacecraft can maneuver to the desired attitude wi...

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Veröffentlicht in:	IEEE transactions on aerospace and electronic systems 2024-10, p.1-11
Hauptverfasser:	Su, Yuhan, Shen, Shaoping, Hu, Zikun, Li, Zhibin
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerospace and electronic systems Angular velocity Attitude control Control barrier function finite-time stability forbidden pointing constraints Instruments Kinematics Lyapunov methods prescribed performance control Quaternions Safety Space vehicles spacecraft attitude reorientation Vectors
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