Optimal Attitude Control of Agile Spacecraft Using Combined Reaction Wheel and Control Moment Gyroscope Arrays
AIAA Modeling and Simulation Technologies Conference
01.01.2016
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
British Library Conference Proceedings | 2016
|Steering the Control Moment Gyroscope Clusters Onboard High-Agile Spacecraft
British Library Conference Proceedings | 2004
|Inertia-Free Spacecraft Attitude Control with Control Moment Gyroscope Actuation
British Library Conference Proceedings | 2012
|