Synthesis of the optimal nonlinear control of spacecraft rotation

Details Synthesis of the optimal nonlinear control of spacecraft rotation Synthesis of the optimal nonlinear control of spacecraft rotation

Jan 1992

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1992kosis..30...52m&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 30, no. 1, Jan.-Feb. 1992, p. 52-59. In Russian.

Physics

Feedback Control, Nonlinear Equations, Optimal Control, Satellite Rotation, Spacecraft Control, Cauchy Problem, Flywheels, Many Body Problem, Spacecraft Maneuvers

Scientific paper

Nonlinear feedback control laws are developed which are intended for the rotation control (reorientation maneuevers) of a spacecraft whose motion is described by nonlinear Euler equations. A system of four bodies consisting of a dynamically nonsymmetrical spacecraft and three flywheels is considered as an example. In the case considered the control is realized via the control moments of the flywheels.

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