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APPLICATION OF DIRECT BTT GUIDANCE LAW BASED ON NONLINEAR INVERSE SYSTEM THEORY TO INTEGRATED FIRE/FLIGHT SYSTEMS(IFFS)
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作者 Ma Xiaojun Zhang Minglian wen chuanyuan(faculty 305, beijing university of aeronautics and astronautics,beijing, china, 100083) 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 1996年第4期305-311,共7页
To counter BTT guidance mode, new relative motion equations of the targetaircraft and the attack aircraft are proposed. The inverse system theory of the nonlinearcontrol is used, and the direct BTT-180 guidance comman... To counter BTT guidance mode, new relative motion equations of the targetaircraft and the attack aircraft are proposed. The inverse system theory of the nonlinearcontrol is used, and the direct BTT-180 guidance command is solved, which can operatethe attack aircraft to automatically complete the flight mission of the preceding stage ofthe terminal weapon delivery, and thus the automatic attack is extended from the stage ofthe terminal weapon delivery to the preceding stage of the terminal weapon delivery. 展开更多
关键词 fire control flight control nonlinear systems inverse system direct BTT guidance law automatic control ATTACK
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