Momentum bias for spacecraft attitude

Advances in the Astronautical Sciences

Volumn 111, Issue , 2002, Pages 35-44

  Rodden, J ^a   McGovern, L ^a   Higham, J ^a   Price, X ^a  

^a California Institute of Technology   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL SYSTEM ANALYSIS; ERRORS; GRAVITATION; MANEUVERABILITY; VECTORS;

SPACECRAFT ATTITUDE;

COMMUNICATION SATELLITES;

EID: 0036372436     PISSN: 00653438     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (10)

1. Dynamic momentum bias for yaw steering
2. Momentum management: Practical applications for operations
3. Analysis and design of WHECON - An attitude control concept
4. Precision attitude control with a single body fixed momentum wheel
5. High pointing accuracy with a momentum bias attitude control system
6. Performance of gravity gradient VCMG systems
7. Dual reaction wheel control of spacecraft pointing
8. Seasat-A attitude control system
9. The attitude stabilization and control system for the communications technology satellite