国防科技大学学报
國防科技大學學報
국방과기대학학보
JOURNAL OF NATIONAL UNIVERSITY OF DEFENSE TECHNOLOGY
2014年
6期
82-87
,共6页
弹道导弹%关机点状态%指数加权递归最小二乘%助推段模型
彈道導彈%關機點狀態%指數加權遞歸最小二乘%助推段模型
탄도도탄%관궤점상태%지수가권체귀최소이승%조추단모형
ballistic missile%burnout states%exponential weighted recursive least square method%boost phase model
在双星预警条件下,将指数加权递归最小二乘算法应用于目标关机点状态估计问题中。通过引入加权因子对目标助推段运动的局部拟线性特性进行描述,从而在一定程度上克服了一般的线性多项式模型难以准确刻画整个助推段运动的难题。通过对助推段目标动力学特性的分析,考察了目标在垂直射面方向上的运动特性。在此基础上,提出了一种更为准确的助推段运动模型。仿真算例表明,所提出的关机点状态估计方法相对于传统的方法具有一定的优越性。
在雙星預警條件下,將指數加權遞歸最小二乘算法應用于目標關機點狀態估計問題中。通過引入加權因子對目標助推段運動的跼部擬線性特性進行描述,從而在一定程度上剋服瞭一般的線性多項式模型難以準確刻畫整箇助推段運動的難題。通過對助推段目標動力學特性的分析,攷察瞭目標在垂直射麵方嚮上的運動特性。在此基礎上,提齣瞭一種更為準確的助推段運動模型。倣真算例錶明,所提齣的關機點狀態估計方法相對于傳統的方法具有一定的優越性。
재쌍성예경조건하,장지수가권체귀최소이승산법응용우목표관궤점상태고계문제중。통과인입가권인자대목표조추단운동적국부의선성특성진행묘술,종이재일정정도상극복료일반적선성다항식모형난이준학각화정개조추단운동적난제。통과대조추단목표동역학특성적분석,고찰료목표재수직사면방향상적운동특성。재차기출상,제출료일충경위준학적조추단운동모형。방진산례표명,소제출적관궤점상태고계방법상대우전통적방법구유일정적우월성。
Under the early warning of two passive satellite-borne sensors,the exponential weighted recursive least square method was applied to the burnout states estimation of ballistic targets.Due to the weighting factor can characterize the local quasi-linearity of the boost phase trajectory of the target,so to some extent the dilemma that generic polynomial cannot handle the whole boost phase of the target can be overcome.Through a dynamic analysis,the kinematic characteristics of boost phase target along the orientation of vertical surface were explored.On that basis,a novel boost phase motion model is proposed,which is more accurate than traditional planar motion model.Simulation results show that the proposed approach is superior to the traditional ones.