Optimum rotational and translational motion control algorithms for spacecraft in the approach stage within a fixed time are synthesized based on the method of analytic construction according to a generalized work criterion in a prediction model version. An analytic solution of the control problem is obtained by proper choice of the form of the prediction model.
Automatic rotational and translational motion control algorithm for spacecraft in the approach stage
Algorithmus für die automatische Steuerung der Rotations- und Translationsbewegung von Raumfahrzeugen in der Annäherungsphase
Soviet Journal of Computer and System Sciences ; 29 , 5 ; 28-39
1991
12 Seiten, 12 Quellen
Aufsatz (Zeitschrift)
Englisch
Nonlinear Optimal Control of Relative Rotational and Translational Motion of Spacecraft Rendezvous
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