Attitude tracking control of a flexible spacecraft under angular velocity constraints
Author:
Affiliation:
1. ONERA, The French Aerospace Lab , Toulouse, France
2. Laboratoire GREYC, UMR CNRS 6072, Université de Caen Basse-Normandie/ENSICAEN , Caen, France
Publisher
Informa UK Limited
Subject
Computer Science Applications,Control and Systems Engineering
Link
https://www.tandfonline.com/doi/pdf/10.1080/00207179.2017.1398841
Reference24 articles.
1. Partial Lyapunov Strictification: Smooth Angular Velocity Observers for Attitude Tracking Control
2. Linear Parameter Varying Analysis of Switched Controllers for Attitude Control Systems
3. Time-response shaping using output to input saturation transformation
4. Attitude Tracking and Disturbance Rejection of Rigid Spacecraft by Adaptive Control
5. Output attitude tracking for flexible spacecraft
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