Kinematic Steering Law for Conically Constrained Torque-Limited Spacecraft Attitude Control
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DOI: 10.2514/1.g002873
Abstract: A novel algorithm for attitude control of a spacecraft subjected to conically constrained inclusion and exclusion regions using a kinematic steering law and a rate-based attitude servo system is presented. The tracking errors are defined… read more here.
Keywords: kinematic steering; control; steering law; torque ... See more keywords