CONTROL SYSTEM OF UNMANNED AIRCRAFT WITH NAVIGATIONAL COMPLEX Russian patent published in 1995 - IPC

FIELD: complex control systems. SUBSTANCE: system has inertial navigational device which includes gyrostabilized platform on which pendulous and string accelerometers are mounted, setting signal generation unit, accelerometer calibration unit, setter of carrier navigational complex parameters, setter of position of platform suspension, setter of certified data of inertial units, certified data correction unit, radio altimeter, altitude and vertical velocity correction unit, radar cursor and control signal generating device which is connected to actuator. Before flight, system is connected to control point fitted on carrier of unmanned aircraft; control point includes navigational complex of carrier, timer and control console. System provides for setting the gyrostabilized platform in inertial navigational complex, calibration of accelerometers, initial control of unmanned aircraft by signals from navigational inertial device followed by control from electronic equipment which is more accurate control equipment. EFFECT: enhanced accuracy of control. 5 cl, 9 dwg