Active Vibration Suppression in Flexible Spacecraft Attitude Maneuver Using Variable Structure Control and Input Shaping Technique
AIAA Guidance, Navigation, and Control Conference and Exhibit
01.01.2005
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Flexible Spacecraft Three Axis Attitude Maneuver by Active Vibration Control
DOAJ | 2009
|Optimal Variable Amplitudes Input Shaping Control for Slew Maneuver of Flexible Spacecraft
Online Contents | 2017
|Optimal Variable Amplitudes Input Shaping Control for Slew Maneuver of Flexible Spacecraft
Springer Verlag | 2021
|Optimal Variable Amplitudes Input Shaping Control for Slew Maneuver of Flexible Spacecraft
Online Contents | 2017
|