Satellite Attitude Control for Emergency Mode Using Reaction Wheels and Magnetic Torquers-Reference-Cited by-同舟云学术

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Satellite Attitude Control for Emergency Mode Using Reaction Wheels and Magnetic Torquers

Published:2023-11-03 Issue: Volume: Page:207-211
ISSN:
Container-title:2023 6th International Conference on Robotics, Control and Automation Engineering (RCAE)
language:
Short-container-title:

Author:

He Yikang¹,Yang Sen²,Lin Shuyu³,He Wen¹,Yang Zhen³

Affiliation:

1. Zhejiang University,Key Laboratory of Advanced Manufacturing Technology of Zhejiang Province,Hangzhou,China

2. School of Astronautics, Harbin Institute of Technology,Harbin,China

3. Shanghai Institute of Spaceflight Control Technology,Shanghai,China

Funder

National Natural Science Foundation of China

National Key R&D Program of China

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/10398736/10398580/10398835.pdf?arnumber=10398835

Reference18 articles.

1. Adaptive Direct Compensation Control Scheme for Spacecraft with Multiple Actuator Faults

2. Sensor fault detection and recovery in satellite attitude control

3. Fault-Tolerant Attitude Control for Spacecraft Under Loss of Actuator Effectiveness

4. Design of Sun-Safe Controllers for Lunar Atmosphere and Dust Environment Explorer

5. Spin-stabilized satellite magnetic attitude control scheme without initial detumbling

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