METHOD FOR FORMATION OF DESCENT PATHS OF AEROBALLISTIC VEHICLE OF REQUIRED CONFIGURATION AT GUIDANCE TO PRESET POINT OF EARTH SURFACE Russian patent published in 2007 - IPC F41G7/22 F41G7/34 

Abstract RU 2296940 C1

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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RU 2 296 940 C1

Authors

Razorenov Gennadij Nikolaevich

Shevtsov Sergej Nikolaevich

Dates

2007-04-10Published

2005-11-11Filed