METHOD OF COMBINED CONTROL OF FLYING VEHICLE

摘要

FIELD: control of unmanned flying vehicles; control of artillery projectiles with homing heads whose flight trajectory consists of three sections: ballistic section, section of flight at constant angle of inclination to longitudinal axis to level (gliding section) and homing section. SUBSTANCE: method consists in limiting angles of inclination of control members (for example, aerodynamic control surfaces) which is effected in its turn due to limiting the input signal to control surface drive in gliding section. Level of signal has magnitude of control signal required for motion of projectile over reference trajectory which is below real trajectories. EFFECT: reduction of the dispersion of artillery projectile in gliding section arising to end of ballistic section of flight due to bringing gliding trajectory to reference trajectory before beginning of homing. 4 dwg