Attitude Control Considering Variable Input Saturation Limit for a Spacecraft Equipped with Flywheels
Chinese Journal of Aeronautics
Chinese Journal of Aeronautics ; 25 , 3 ; 437-445
01.06.2012
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Spacecraft attitude variable performance control method considering input saturation
Europäisches Patentamt | 2024
|Line-of-sight pointing control of spacecraft actuated by two flywheels considering input saturation
Online Contents | 2013
|Spacecraft Attitude Tracking and Energy Storage Using Flywheels
British Library Online Contents | 2005
|Integrated Power and Attitude Control with Spacecraft Flywheels and Control Moment Gyroscopes
Online Contents | 2004
|