Space subsystems design: (navigation, control, structure and…)
Attitude and Vibration Control of a Flexible Spacecraft Using Hybrid Adaptive Super-Twisting Non-Singular Terminal Sliding Mode Control

Valiollah Shahbahrami; Milad َAzimi; َAlireza Alikhani

Volume 16, Issue 4 , December 2023, , Pages 1-13

Abstract
  In this paper, a robust adaptive hybrid control approach based on a combination of super-twisting and non-singular terminal sliding mode control (STNSMC) approaches for vibration and attitude control of a flexible spacecraft with fully coupled dynamic is developed. The proposed adaptation law eliminates ...  Read More