State feedback ℋ/sub ∞/-suboptimal control of a rigid spacecraft

DOI10.1109/9.618253zbMath0889.93023OpenAlexW1487914696MaRDI QIDQ4358001

M. Dalsmo, Olav Egeland

Publication date: 28 September 1997

Published in: IEEE Transactions on Automatic Control (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1109/9.618253

zbMATH Keywords

orthogonal groupEuler anglesHamilton-Jacobi inequalityrigid spacecraft\({\mathcal H}_ \infty\)-control problem

Mathematics Subject Classification ID

Application models in control theory (93C95) (H^infty)-control (93B36)

Related Items (10)

Design of a steering control law for an autonomous underwater vehicle using nonlinear \(\mathscr {H}_{\infty }\) state feedback technique ⋮ Inverse optimal adaptive backstepping control for spacecraft rendezvous on elliptical orbits ⋮ H _∞ inverse optimal attitude tracking on the special orthogonal group SO (3) ⋮ Global set stabilization of the spacecraft attitude control problem based on quaternion ⋮ Adaptive tracking control using synthesized velocity from attitude measurements ⋮ Trading robustness with optimality in nonlinear control ⋮ Inverse optimal sliding mode control of spacecraft with coupled translation and attitude dynamics ⋮ Global set stabilisation of the spacecraft attitude using finite-time control technique ⋮ Robust stabilization of the angular velocity of a rigid body ⋮ Robust attitude tracking on the special orthogonal group \(SO(3)\) using PD-type state feedback and linear matrix inequalities

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