Active Vibration Suppression in Flexible Spacecraft Attitude Maneuver Using Variable Structure Control and Input Shaping Technique
AIAA Guidance, Navigation, and Control Conference and Exhibit
2005-01-01
Conference paper
Electronic Resource
English
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
|