FIELD: guidance control of flight vehicles, applicable for formation of various descent paths of the preset configuration in the process of guidance of aeroballistic vehicle to the preset point of the earth surface (target point).
SUBSTANCE: the method consists in formation of spiral descent path of the flight vehicle of various configuration. An the process of control of the flight vehicle descent programmed rotation of the required direction of the vector of the flight vehicle terminal velocity in the generating line of the right circular cone with the peak in the target point in the direct or reversed direction with a constant or variable period of rotation is accomplished.
EFFECT: realized maneuvering capabilities of descending aeroballistic vehicles by formation of various descent paths.
3 dwg
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Authors
Dates
2007-04-10—Published
2005-11-11—Filed