Integrated Design of Normal and Fault Modes for Spacecraft Control Systems
Author:
Affiliation:
1. Beijing Institute of Spacecraft System Engineering,China Academy of Space Technology,Beijing,P. R. China,100094
2. Sun Yat-sen University,School of Aeronautics and Astronautic,Guangzhou,P. R. China,510006
Funder
China Postdoctoral Science Foundation
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10243163/10243123/10243259.pdf?arnumber=10243259
Reference21 articles.
1. H/sub 2/-norm optimization with constrained dynamic output feedback controllers: decentralized and reliable control
2. Reliable Control of Discrete-Time Piecewise-Affine Time-Delay Systems via Output Feedback
3. Reliable fuzzy output feedback control of nonlinear parabolic distributed parameter systems with sensor faults1
4. Fuzzy-Model-Based Reliable Static Output Feedback $\mathscr{H}_{\infty }$ Control of Nonlinear Hyperbolic PDE Systems
5. Adaptive Reliable $H_{\infty }$ Optimization Control for Linear Systems With Time-Varying Actuator Fault and Delays
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