Disturbance observer-based adaptive integral sliding mode control for rigid spacecraft attitude maneuvers
Author:
Affiliation:
1. School of Automation, Beijing Institute of Technology, Beijing, China
2. Key Laboratory for Intelligent Control & Decision of Complex Systems, Beijing Institute of Technology, Beijing, China
Publisher
SAGE Publications
Subject
Mechanical Engineering,Aerospace Engineering
Link
http://journals.sagepub.com/doi/pdf/10.1177/0954410012464588
Reference20 articles.
1. Variable-structure control of spacecraft large-angle maneuvers
2. Robust Tracking Control Design for Spacecraft Under Control Input Saturation
3. Sliding-mode adaptive attitude controller design for spacecrafts with thrusters
4. Variable-structure control of spacecraft attitude maneuvers
5. Exponential Time-varying Sliding Mode Control for Large Angle Attitude Eigenaxis Maneuver of Rigid Spacecraft
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