Skip to main content

Research Repository

Advanced Search

Design procedure of chattering attenuation sliding mode attitude control of a satellite system

Nemati, Hamidreza; Hokamoto, Shinji

Authors

Shinji Hokamoto



Abstract

This study presents a design procedure for a new robust nonlinear control algorithm based on the theory of the terminal sliding mode (TSM) to control the attitude of a satellite system. Since the traditional TSM controllers include a discontinuous function, a significant problem called chattering can occur. In this paper, a methodology for designing a new switching function is discussed to alleviate this drawback over time. Besides, to highlight the robustness of the proposed method against uncertainties, a satellite with three pairs of thrusters subject to parameter variation is simulated.

Presentation Conference Type Conference Paper (Published)
Conference Name 24th AAS/AIAA Space Flight Mechanics Meeting
Start Date Jan 26, 2014
End Date Jan 30, 2014
Acceptance Date Jan 26, 2014
Publication Date 2014
Deposit Date Apr 21, 2020
Volume 152
ISBN 9780877036111
Public URL https://uwe-repository.worktribe.com/output/5883475