Linear quadratic control for spacecraft large-angle maneuvers

A. I. Shestoperov, S. S. Tkachev


Abstract: The inertial stabilization problem of a spacecraft moving in a geostationary orbit is considered. Linear quadratic control laws which realize large-angle maneuvers are obtained by means of corresponding selection of algebraic Riccati equation stabilizing solutions.

Keywords: inertial stabilization, PD-regulator, linear quadratic control, algebraic Riccati equation.

DOI: 10.20948/prepr-2019-142