A near-optimal minimum-time guidance law to a fixed point under a terminal angular manifold is developed. The planar case and the spatial case are separately considered. The problems are solved in several stages with increased level of complexity: from the simple case of a constant speed with a fixed terminal angular direction (Dubins problem), through the case of a constant speed with a terminal conical manifold, to the more general case of atmospheric flight with a terminal conical manifold.


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    Title :

    Near-Optimal Minimum-Time Guidance Under Spatial Angular Constraint in Atmospheric Flight


    Contributors:

    Published in:

    Publication date :

    2016-07-01




    Type of media :

    Conference paper , Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English





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