| 摘要 |
FIELD: space.SUBSTANCE: invention relates to space engineering and can be used when generating control signals for switching engine of unmanned aerial vehicle (UAV) when performing spatial manoeuvre on ballistic flight path segment. Method includes storing up to start of a multi-stage launch vehicle (LV) an electronic-digital flight mission, measuring kinematic parameters of active portion of flight path of last stage of multi-stage rocket, storing measured parameters of active portion of flight path of a multi-stage rocket flight of the last stage, measuring and storing kinematic parameters of centre of mass of cosmic movement UAV and time since formation of control signal for separating space UAV from the last stage of launch vehicle, comparing measured values of kinematic parameters of motion of centre mass of space UAV with calculated values of flight task, generating a signal of possible discrepancy between measured and given in flight task kinematic parameters of space UAV motion centre of mass towards its reduction to zero, generating a control signal of flight task for switching correction engine of space UAV to perform an avoidance manoeuvre.EFFECT: generation of control signals for switching engine of space unmanned aerial vehicle (UAV) in spatial manoeuvre on ballistic flight path segment.1 cl, 1 dwg. |
