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GPS AND INS INTEGRATED NAVIGATION SYSTEM CAPABLE OF LOADING A GPS GUIDING KIT FOR A GUIDANCE CONTROL DEVICE
GPS AND INS INTEGRATED NAVIGATION SYSTEM CAPABLE OF LOADING A GPS GUIDING KIT FOR A GUIDANCE CONTROL DEVICE
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机译：GPS和INS集成导航系统，可为制导控制装置装载GPS制导套件
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摘要
PURPOSE: A GPS(global positioning system) and INS(inertial navigation system) integrated navigation system for loading a GPS guiding kit is provided to accurately strike a target by attaching the GPS guiding kit on a conventional bomb.;CONSTITUTION: A telemetry transmission system(100) of a guided missile provides GPS and INS integrated navigation information including the posture, the speed and the position of the guided missile to the ground. A ground telemetry reception system(200) receives the GPS and INS integrated navigation information. A fight control unit(300) controls arrival and departure, flight direction, flight altitude and speed. A pilot display unit(400) communicates using a data transmission card embedded in the flight control device and a wireless data link.;COPYRIGHT KIPO 2013;[Reference numerals] (100) Telemetry(measurement rocket); (200) Telemetry(ground); (300) Fight control unit; (310) Data transmission card(DTC); (320) Guide control card(GCC); (330) Inertia navigation card(INC); (400) Pilot demonstration unit(PDU); (450) Inertia measurement unit(IMU); (AA) GPS antenna; (BB) GPS RF signal; (CC) GPS navigation information before drop; (DD) Integrated navigation system; (EE) GPS navigation information after drop; (FF) Inertia data; (GG) GPS/INS integrated navigation system
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