Time-optimal slewing of flexible spacecraft

DOI10.2514/3.20844zbMath0775.93137OpenAlexW2083209753MaRDI QIDQ4014674

Joseph Z. Ben-Asher, John A. Burns, Eugene M. Cliff

Publication date: 18 October 1992

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

Full work available at URL: http://hdl.handle.net/10919/53910

zbMATH Keywords

time-invariant

Mathematics Subject Classification ID

Model systems in control theory (93C99)

Related Items (9)

SPACE-TIME SPECTRAL ELEMENT METHOD FOR OPTIMAL SLEWING OF A FLEXIBLE BEAM ⋮ Time‐energy optimal control of vector controlled induction motor ⋮ Frequency and Time Domain Analysis of an Aeroelastic Wing Multiple Component Structure ⋮ Nonlinear attitude control scheme with disturbance observer for flexible spacecrafts ⋮ Optimal limited-rate slewing of a flexible spacecraft ⋮ An anti-disturbance PD control scheme for attitude control and stabilization of flexible spacecrafts ⋮ Nonlinear feedback control of slewing beams ⋮ Nonlinear minimum-time control with pre- and post-actuation ⋮ Optimal vibration control of flexible spacecraft during a minimum-time maneuver

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