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.


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    Title :

    Controlling of a return space vehicle along transition trajectories in atmosphere


    Contributors:

    Published in:

    Publication date :

    2015-04-01


    Size :

    8 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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