基于闭路制导的弹道导弹发射诸元的仿真算法  

Simulation Algorithm Basic Firing Data of Ballistic Missiles Based on Close-Loop Guidance Law

作　　者：黎国保 耿宝亮[2] 

机构地区：[1]海军驻平坝地区航空军事代表室,贵州平坝561102 [2]海军航空工程学院控制工程系,山东烟台264001

出　　处：《海军航空工程学院学报》2011年第2期212-218,共7页Journal of Naval Aeronautical and Astronautical University

基　　金：总装备部“十一五”预研项目(51319010302)

摘　　要：提出了一种基于闭路制导的弹道导弹的发射诸元算法。给定发射点与瞄准点的地理位置,以压低弹道为目标,通过一种迭代方法求解关机点弹道倾角,并基于地球引力级数展开模型提出了一种虚拟目标的快速计算方法,以主动段弹道平面和被动段弹道平面二面角为指标完成了发射方位角的迭代计算,最后通过仿真算例论证了该算法的可行性。An effective approach for computing the basic firing data of ballistic missiles based on close-loop guidance law was presented.If the launch position and aiming position were given,velocity obliquity could be gotten by iterative method aiming at depressing trajectory.Based on gravitational series model,a new scheme was proposed to calculate virtual target.In the process of calculating optimal azimuth angle,dihedral angel was introduced into the iterative algorithm which improved computing velocity with no loss of firing accuracy.Finally,the feasibility of this approach was demonstrated by numerical simulation study.

关 键 词：发射诸元 弹道导弹 闭路制导 仿真 

分 类 号：TP391.9[自动化与计算机技术—计算机应用技术] TJ760[自动化与计算机技术—计算机科学与技术]