METHOD OF CONTROL OVER CARRIER ROCKET BOOST PHASE Russian patent published in 2013 - IPC B64G1/26 F42B15/00 

FIELD: transport.

SUBSTANCE: invention relates to rocketry. Proposed method consists in deflection of midflight engine swing part in preset plane of jet deflection plane with allowance for periodic computation of command signal in response to midflight engine swing part deflection subject to program angle, deflection and rate of deflection of carrier rocket distinguished point from launcher vertical axis, carrier rocket pitch rate and angle and simultaneous stabilisation of carrier rocket angular position in the plane perpendicular to preset one. Said deflection of midflight engine swing part is performed by assuming said program angle of said deflection of midflight engine swing part and command signal gain with respect to distinguished point deflection and deflection rate from launcher vertical axis by preset laws from periodically measured elevation above launcher horizontal plane, said distinguished points is assumed to be the center of said swing part.

EFFECT: longer life of launcher.

4 dwg