New Penalty Functions and Optimal Control Formulation for Spacecraft Attitude Control Problems

DOI10.2514/2.4093zbMath0894.49021OpenAlexW1999428181MaRDI QIDQ4370717

Hanspeter Schaub, John L. Junkins, Rush D. III Robinett

Publication date: 28 January 1998

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

Full work available at URL: https://doi.org/10.2514/2.4093

zbMATH Keywords

modified Rodrigues parametersswitchingattitude penalty functionspacecraft optimal control

Mathematics Subject Classification ID

Differential games and control (49N70) Free motion of a rigid body (70E15) Pursuit and evasion games (49N75)

Related Items (5)

Minimal energy maneuvering control of a rigid spacecraft with momentum transfer ⋮ Geometric structure-preserving optimal control of a rigid body ⋮ Orientation and kinematics of rotation: quaternionic and four-dimensional skew-symmetric operators, equations, and algorithms ⋮ Optimal control of satellite attitude and its stability based on quaternion parameters ⋮ Distributed fixed-time attitude coordinated tracking for multiple rigid spacecraft via a novel integral sliding mode approach

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