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.
Near-Optimal Minimum-Time Guidance Under Spatial Angular Constraint in Atmospheric Flight
Journal of Guidance, Control, and Dynamics ; 39 , 7 ; 1563-1577
2016-05-30
15 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Near-Optimal Minimum-Time Guidance Under Spatial Angular Constraint in Atmospheric Flight
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