Robust \(H_{\infty}\) control of spacecraft rendezvous on elliptical orbit

DOI10.1016/J.JFRANKLIN.2012.08.005zbMath1300.93065OpenAlexW2280102090MaRDI QIDQ473424

Guang-Ren Duan, Kok Lay Teo, Xiang-Yu Gao

Publication date: 24 November 2014

Published in: Journal of the Franklin Institute (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.jfranklin.2012.08.005

zbMATH Keywords

robust \(H_{\infty}\) controlfast multi-shot algorithmRiccati differential equation (RDE)spacecraft rendezvous on elliptical orbitstabilizable controller

Mathematics Subject Classification ID

Sensitivity (robustness) (93B35) Nonlinear systems in control theory (93C10) (H^infty)-control (93B36) Variable mass, rockets (70P05) Numerical methods for initial value problems involving ordinary differential equations (65L05) Control/observation systems governed by ordinary differential equations (93C15)

Related Items (5)

Inverse optimal adaptive backstepping control for spacecraft rendezvous on elliptical orbits ⋮ Attitude stabilization control of a quadrotor UAV by using backstepping approach ⋮ Optimal nonlinear feedback control of spacecraft rendezvous with finite low thrust between libration orbits ⋮ Output feedback gain scheduled control of actuator saturated linear systems with applications to the spacecraft rendezvous ⋮ An optimal control approach to spacecraft rendezvous on elliptical orbit

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