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一种瞬时圆周加速度制导律设计
引用本文:李伟,王志刚,蒋奇英.一种瞬时圆周加速度制导律设计[J].飞行力学,2012,30(3):272-275.
作者姓名:李伟  王志刚  蒋奇英
作者单位:1. 西北工业大学航天学院,陕西西安,710072
2. 第二炮兵青州士官学校202教研室,山东青州,262500
摘    要:为了保证导弹攻击目标的精确性,根据平面弹道的几何特性,设计了一种输出指令为过载的瞬时圆周制导律.描述了瞬时圆周加速度制导律原理,详细推导了制导方程.利用导弹质心和目标质心的位置及速度信息,得出导弹攻击目标的过载制导指令,并进行了弹道仿真.仿真结果表明,所设计的瞬时圆周加速度制导律不仅能够保证导弹准确命中目标,而且弹道平...

关 键 词:导弹  制导律  瞬时圆周加速度  弹道仿真

Design of instantaneous circular acceleration guidance law
LI Wei , WANG Zhi-gang , JIANG Qi-ying.Design of instantaneous circular acceleration guidance law[J].Flight Dynamics,2012,30(3):272-275.
Authors:LI Wei  WANG Zhi-gang  JIANG Qi-ying
Institution:1.College of Astronautics,Northwestern Polytechnical University,Xi’an 710072,China; 2.202 Staff Room,The Second Artillery NCO School,Qingzhou 262500,China)
Abstract:In order to ensure the accuracy of the missile against target,we design an instantaneous circular guidance law according to the geometric properties of flat trajectory;the guidance law’s output command is an overload.The principle of instantaneous circular acceleration guidance law is described and the detailed derived equations of guidance law are also given.We obtain guidance overload command utilizing the centroid position and centroid velocity information of the missile and target when the missile attacks a target,we make a trajectory simulation finally.The simulation results illustrate that the instantaneous circular acceleration guidance law is not only hitting the target but also trajectory straight.
Keywords:missile  guidance law  instantaneous circular acceleration  ballistic simulation
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