Adaptive Minimal Control Synthesis for Satellite Attitude Control in Presence of Propellant Sloshing and Flexible Appendices
Author:
Affiliation:
1. ONERA,Département Traitement de l'information et systèmes, DTIS,Toulouse,France
2. CNES,Toulouse,France
Funder
CNES
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/9837955/9837961/09838221.pdf?arnumber=9838221
Reference16 articles.
1. Empirical studies of an MRAC algorithm with minimal controller synthesis
2. Robustness of a minimal controller synthesis algorithm
3. Design of multivariable adaptive model following control systems
4. The Effects of Propellant Slosh Dynamics on the Solar Dynamics Observatory
5. Minimal LFT form of a spacecraft built up from two bodies
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