Nonlinear H∞ robust control for satellite large angle attitude maneuvers

Proceedings of the American Control Conference

Volumn 2, Issue , 2001, Pages 1357-1362

  Show, L L ^a   Juang, J C ^a   Yang, C D ^a  

^a NATIONAL CHENG KUNG UNIVERSITY   (Taiwan)

Author keywords

Large angle attitude maneuvers; Nonlinear H state feedback

Indexed keywords

COMPUTER SIMULATION; CONTROL SYSTEM ANALYSIS; CONTROL SYSTEM SYNTHESIS; FEEDBACK CONTROL; NUMERICAL METHODS; ROBUSTNESS (CONTROL SYSTEMS); SATELLITES; SPACECRAFT; SYSTEM STABILITY;

DISTURBANCE REJECTION; SATELLITE LARGE ANGLE ATTITIUDE MANEUVERS; THRUSTER;

NONLINEAR CONTROL SYSTEMS;

EID: 0034857723     PISSN: 07431619     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (11)

1. Attitude control for large angle maneuvers
2. Nonlinear adaptive attitude control of spacecraft
3. Robust attitude stabilization of spacecraft using nonlinear quaternion feedback
4. Quaternion feedback for spacecraft large angle maneuvers
5. ∞ control and its applications to rigid spacecraft
6. ∞ flight control of general six degree-of-freedom motions
7. ∞ and mixed control of spacecraft
8. ∞ control problem for robust tracking of robotic system
9. ∞ control
10. ∞ control via measurement feedback for affine nonlinear system
11. ∞ control via measurement feedback