An optimization result with application to optimal spacecraft reaction wheel orientation design

Proceedings of the American Control Conference

Volumn 2, Issue , 2001, Pages 1473-1478

  Bayard, D S ^a  

^a CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

OPTIMAL SPACECRAFT REACTION WHEEL ORIENTATION DESIGN; THREE REACTION WHEEL ACTUATOR;

ACTUATORS; CONFORMAL MAPPING; CONSTRAINT THEORY; MATRIX ALGEBRA; PARAMETER ESTIMATION; SPACECRAFT; TORQUE;

OPTIMIZATION;

EID: 0034842537     PISSN: 07431619     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/ACC.2000.876746     Document Type: Conference Paper

References (10)

1. An optimization approach to orienting three spacecraft reaction wheel actuators with application to the Europa Orbiter. Jet propulsion laboratory
2. Tres observaciones sobre el algebra lineal
3. Momentum vector considerations in wheel-jet satellite control system design
4. Precision three-axis attitude control via skewed reaction wheel momentum management
5. Sun-tracking commands and reaction wheel sizing with configuration optimization