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Trajectory design and simulation in injection phase for hyper-velocity kinetic energy missile 被引量:1
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作者 于剑桥 梅跃松 韩朝 《Journal of Beijing Institute of Technology》 EI CAS 2011年第1期18-22,共5页
A movement law of laser beam facula is designed for the injection trajectory of hyper-ve- locity kinetic energy missile to eliminate the influence of motor exhaust smoke on laser signal trans mission. Taking guidance... A movement law of laser beam facula is designed for the injection trajectory of hyper-ve- locity kinetic energy missile to eliminate the influence of motor exhaust smoke on laser signal trans mission. Taking guidance loop of hyper velocity kinetic energy missile as plant, a closed loop control system with desired step response characteristics is constructed and the movement law of laser beam facula for the missile injection trajectory is designed based on the output signal of the closed loop controller under a step input. Six degree of freedom trajectory simulations show that by the guidance of the laser beam facula moving with designed law, the missile can finish transition from the initial trajectory to a stable tracking trajectory without overshoot within the required time. 展开更多
关键词 trajectory design trajectory simulation missile control hyper velocity kinetic energymissile
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