发明名称 TEST SYSTEM FOR SPACE LAUNCH VEHICLE
摘要 PURPOSE: The projectile check is proceed through the remote control of the subsystem check of the main control module of the move mode rack shape and projectile. Stability can be secured to the utmost from environment. CONSTITUTION: A projectile diagnostic system comprises a main control module(110). The main control module is formed into the move mode rack shape. The main control module comprises a DC offset control part(111), a digital communications controller(112), an analog communications controller(113), a serial communications controller(114), and a microprocessor(115). The DC offset control part supplies the DC power supply to each subsystem of the projectile(10). The digital communications controller is proceed transmitting and receiving of the digital command of the subsystem of projectile. The analog communications controller is proceed transmitting and receiving of the analog command of the subsystem of projectile. It monitors the state of the subsystem of projectile and the serial communications controller controls.
申请公布号 KR20110073983(A) 申请公布日期 2011.06.30
申请号 KR20090130803 申请日期 2009.12.24
申请人 KOREA AEROSPACE RESEARCH INSTITUTE 发明人 KIM, KWANG SOO;LEE, SOO JIN;SEO, JIN HO;HWANG, SEUNG HYUN;JI, KI MAN;CHUNG, EUI SEUNG;PARK, JEONG JOO;CHO, GWANG RAE
分类号 G01M99/00;B64G5/00 主分类号 G01M99/00
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