Feedback linearization and solar pressure satellite attitude control

IEEE Transactions on Aerospace and Electronic Systems

Volumn 32, Issue 2, 1996, Pages 732-741

  Singh, Sahjendra N ^a   Yim, Woosoon ^a  

^a University of Nevada Las Vegas   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CLOSED LOOP CONTROL SYSTEMS; COMPUTER SIMULATION; DIFFERENTIAL EQUATIONS; ERRORS; MANEUVERABILITY; ROBUSTNESS (CONTROL SYSTEMS); SOLAR RADIATION;

CLOSED LOOP SYSTEM; FEEDBACK LINEARIZATION; FOURTH ORDER LINEAR DIFFERENTIAL EQUATION; GRAVITY GRADIENT TORQUE; INTEGRAL ERROR FEEDBACK; REFLECTOR COLLECTOR SYSTEM; SOLAR RADIATION PRESSURE;

SATELLITES;

EID: 0030128063     PISSN: 00189251     EISSN: None     Source Type: Journal    
DOI: 10.1109/7.489516     Document Type: Article

References (21)

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