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Time efficient sliding mode controller based on Bang–Bang logic for satellite attitude control

  • Published:2018-04 Issue: Volume:75 Page:342-352
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Li You,Ye DongORCID,Sun Zhaowei

Funder

National Natural Science Foundation of China

China Postdoctoral Science Foundation

Open Fund of National Defense Key Discipline Laboratory of Micro-Spacecraft Technology

Heilongjiang Postdoctoral Fund

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference24 articles.

1. A structure simple controller for satellite attitude tracking maneuver;Xiao;IEEE Trans. Ind. Electron.,2017

2. Tracking control of robotic manipulators with uncertain kinematics and dynamics;Xiao;IEEE Trans. Ind. Electron.,2016

3. Velocity-free fault tolerant and uncertainty attenuation control for a class of nonlinear systems;Xiao;IEEE Trans. Ind. Electron.,2016

4. Robust sliding mode controller design for globally fast attitude tracking of target spacecraft;Wu;Int. J. Innov. Comput. Inf. Control,2011

5. Robust attitude maneuver control of spacecraft with reaction wheel low-speed friction compensation;Wu;Aerosp. Sci. Technol.,2015

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