Optimal nonlinear feedback control for spacecraft attitude maneuvers

DOI10.2514/3.20073zbMath0596.93027OpenAlexW2068432135MaRDI QIDQ3728750

John L. Junkins, Connie K. Carrington

Publication date: 1986

Published in: Journal of Guidance, Control, and Dynamics (Search for Journal in Brave)

Full work available at URL: http://hdl.handle.net/10919/74666

zbMATH Keywords

momentum transferinternal control torqueslarge-angle, nonlinear spacecraft attitude maneuversPolynomial feedback controls

Mathematics Subject Classification ID

Nonlinear systems in control theory (93C10) Orbital mechanics (70M20) Control/observation systems governed by ordinary differential equations (93C15)

Related Items (15)

Minimal energy maneuvering control of a rigid spacecraft with momentum transfer ⋮ Simultaneous maneuver and vibration suppression of flexible spacecraft ⋮ Analytical computation of differential equations involved in dynamical nonlinear optimal problems ⋮ Spacecraft Anti‐Unwinding Attitude Control Using Second‐Order Sliding Mode ⋮ Continuous precise predefined-time attitude tracking control for a rigid spacecraft ⋮ Robust time-delay control of multimode systems ⋮ Robust finite-time control allocation in spacecraft attitude stabilization under actuator misalignment ⋮ Trajectory generation under constraints by linearization method ⋮ Fixed-time control for high-precision attitude stabilization of flexible spacecraft ⋮ Finite-time control for attitude tracking maneuver of rigid satellite ⋮ Global set stabilization of the spacecraft attitude control problem based on quaternion ⋮ Optimal vibration control of flexible spacecraft during a minimum-time maneuver ⋮ Time-Optimal De-tumbling Control of a Rigid Spacecraft ⋮ ANALYTIC-APPROXIMATE SOLUTION FOR A CLASS OF NONLINEAR OPTIMAL CONTROL PROBLEMS BY HOMOTOPY ANALYSIS METHOD ⋮ Robust and optimal attitude control of spacecraft with disturbances

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