Abstract For an interception strategy of a removable target by a return space vehicle (RSV), we propose a structure of the control law by the aerodynamic efficiency that determines a chain of the three standard trajectories: nosing-up–free flight–nosing-down. A solution of the terminal problem is to determine numerical values of the control parameters that define moments to switch the RSV flight from one standard trajectory to another.
Analytical construction of interception trajectories in atmosphere
Russian Aeronautics (Iz VUZ) ; 59 , 1 ; 15-22
01.01.2016
8 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Analytical construction of interception trajectories in atmosphere
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