Optimal Output Feedback Controllers for Spacecraft Attitude Tracking
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Publication:5416957
DOI10.1002/asjc.615zbMath1286.93078OpenAlexW1513441347MaRDI QIDQ5416957
Publication date: 15 May 2014
Published in: Asian Journal of Control (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1002/asjc.615
extended state observerdisturbance estimatorstate-dependent Riccati equation (SDRE)attitude tracking controloptimal Lyapunov approach
Feedback control (93B52) Applications of optimal control and differential games (49N90) Variable mass, rockets (70P05) Control/observation systems governed by ordinary differential equations (93C15)
Related Items (6)
Optimal Tracking for State-Dependent Coefficient Factorized Nonlinear Systems ⋮ On the Design of Observer for Nonlinear Time-Delay Systems ⋮ Reduced‐order Observer for State‐dependent Coefficient Factorized Nonlinear Systems ⋮ Inverse optimal control via diagonal stabilization applied to attitude tracking of a reusable launch vehicle ⋮ The Synthesis of the Proportional-Differential Regulators for the Systems with Fixed Ends of Trajectories Under Two-Sided Constraints on Control Values ⋮ Adaptive Fuzzy PD+ Control for Attitude Maneuver of Rigid Spacecraft
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