Abstract We present the results of constructing a flight control law for a return space vehicle (RSV) along transition trajectories in atmosphere by using a method of analytical construction of composite trajectories from standard periods. A terminal problem is resolved, in which three final coordinates are specified, namely, altitude, trajectory angle, and distance.
Controlling of a return space vehicle along transition trajectories in atmosphere
Russian Aeronautics (Iz VUZ) ; 58 , 2 ; 152-159
2015-04-01
8 pages
Article (Journal)
Electronic Resource
English
Controlling of a return space vehicle along transition trajectories in atmosphere
Online Contents | 2015
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