Simulation result showed that response time of missile was reduced and guidance accuracy was accordingly increased by side jet and aerodynamic compound control manner in terminal guidance.

 
  • 通過(guò)仿真研究表明:在末制導階段,采用燃氣動(dòng)力/氣動(dòng)力復合控制方式可提高導彈的快速性,進(jìn)而提高導彈的制導控制精度。
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