A complete analytical synthesis of a control maximizing response speed is given for a one-dimensional problem of the meeting of two spacecraft at the approach stage with allowance for varying mass. The optimal synthesizing functions are found in the form of analytical expressions for the dependence on the coordinates of the three-dimensional phase vector.
Synthesis of a control system that is optimal with respect to response speed
Synthese eines Regelsystems, das optimal im Hinblick auf Antwortgeschwindigkeit ist.
Engineering Cybernetics ; 14 , 3 ; 145-155
1976
11 Seiten, 2 Quellen
Article (Journal)
English
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