| 摘要 |
FIELD: applicable in aviation and rocketry. SUBSTANCE: the control system of a pilotless flight vehicle has an engine control unit, altimeter, gyroinertial system with attitude transducers and accelerometers, roll-rate pick-ups, computer, adders of control signals of pitch, heading and bank, unit of kinematic arrangement and invertors, containing adders of control actuators and invertors, control actuators, delay units, storage, comparators, OR gate, AND gates, units of modulus determination, derivative computation unit, multiplier unit, adders, key, adder of liquidation signal and a flight termination subsystem. EFFECT: enhanced efficiency of the on-board control system of pilotless flight vehicle in the conditions of training-combat launches; provided a fall of the flight vehicle within the preset limits of providing grounds, in case of various failures of subsystems of the pilotless flight vehicle. 4 dwg |
