Non-fragile robustH∞control for uncertain spacecraft rendezvous system with pole and input constraints
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Publication:5745594
DOI10.1080/00207179.2012.669848zbMath1282.93103OpenAlexW1968293031MaRDI QIDQ5745594
Guanren Duan, Kok Lay Teo, Xiang-Yu Gao
Publication date: 30 January 2014
Published in: International Journal of Control (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1080/00207179.2012.669848
Sensitivity (robustness) (93B35) (H^infty)-control (93B36) Variable mass, rockets (70P05) Pole and zero placement problems (93B55) Control/observation systems governed by ordinary differential equations (93C15)
Related Items (8)
Inverse optimal adaptive backstepping control for spacecraft rendezvous on elliptical orbits ⋮ Autonomous spacecraft rendezvous with finite time convergence ⋮ Multi-objective output feedback control for autonomous spacecraft rendezvous ⋮ Output feedback robust \(H_\infty\) control for spacecraft rendezvous system subject to input saturation: A gain scheduled approach ⋮ Robust H∞ dynamic output feedback control for spacecraft rendezvous with poles and input constraint ⋮ Discrete gain scheduling control approach to elliptical orbit rendezvous system with actuator saturation ⋮ Fault-tolerant sampled-data control of flexible spacecraft with probabilistic time delays ⋮ Pure delayed non-fragile control for offshore steel jacket platforms subject to non-linear self-excited wave force
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