Extended state filter‐based velocity‐free finite‐time attitude control of spacecraft

This brief presents a finite‐time output feedback control scheme for the velocity‐free attitude stabilization of rigid spacecraft under inertia uncertainties and disturbances. Note that either the finite‐time velocity observer or the finite‐time extended state observer contains the control torques,...

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Veröffentlicht in:	International journal of robust and nonlinear control 2024-05, Vol.34 (8), p.5540-5552
Hauptverfasser:	Yao, Qijia, Li, Qing, Xi, Yaming, Jahanshahi, Hadi
Format:	Artikel
Sprache:	eng
Schlagworte:	Angular velocity Attitude stability attitude stabilization Control systems extended state filter Feedback control finite‐time control Output feedback output feedback control Spacecraft Spacecraft attitude control Stability analysis State observers System theory Systems theory Torque Transient performance Uncertainty Velocity
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