Answers are grounded in this paper and cite their sources.
The problem of reducing the angular velocities of a space vehicle to zero is considered. The required control torques are found as functions of the angular momenta. Both linear and nonlinear time-invariant feedback control systems are determined. The method of solution is based on the "inverse problem" of optimal control.
No takes yet. Share an insight, caveat, or question.
Debs et al. (1969) studied this question.
Synapse has enriched 10 related papers. Consider them for comparative context: