Nonlinear Adaptive Control of Spacecraft Maneuvers

DOI10.2514/2.4192zbMath0905.93033OpenAlexW2042504856MaRDI QIDQ4396033

Maruthi Ram Akella, John L. Junkins, Rush D. III Robinett

Publication date: 11 June 1998

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

Full work available at URL: https://semanticscholar.org/paper/c6498eb7786bafbc524198827b7b397ff93fd0d7

zbMATH Keywords

saturation constraintinverse dynamicsminimum-time maneuvers of a spacecraftunknown inertia

Mathematics Subject Classification ID

Application models in control theory (93C95) Adaptive control/observation systems (93C40) Free motion of a rigid body (70E15)

Related Items (6)

Attitude and altitude control of trirotor UAV by using adaptive hybrid controller ⋮ Spacecraft Anti‐Unwinding Attitude Control Using Second‐Order Sliding Mode ⋮ Robust finite-time control allocation in spacecraft attitude stabilization under actuator misalignment ⋮ Null‐space‐based optimal control reallocation for spacecraft stabilization under input saturation ⋮ Rigid body attitude tracking without angular velocity feedback ⋮ Velocity-free fault-tolerant control allocation for flexible spacecraft with redundant thrusters

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