Adaptive Control on SE(3) for Spacecraft Pose Tracking With Harmonic Disturbance and Input Saturation
Author:
Affiliation:
1. Research Center of Satellite Technology, Harbin Institute of Technology, Harbin, China
Funder
National Natural Science Foundation of China
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Subject
Electrical and Electronic Engineering,Aerospace Engineering
Link
http://xplorestaging.ieee.org/ielx7/7/9915531/09751389.pdf?arnumber=9751389
Reference48 articles.
1. Finite-time relative orbit-attitude tracking control for multi-spacecraft with collision avoidance and changing network topologies
2. Adaptive prescribed performance control for flexible spacecraft with input saturation and actuator misalignment
3. Output Regulation Control for Satellite Formation Flying Using Differential Drag
4. Attitude Control for Flexible Spacecraft With Disturbance Rejection
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