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考虑地球非球形摄动的固体动能拦截器助推段最优控制方案研究
引用本文:潘伟,路长厚,冯维明,葛培琪.考虑地球非球形摄动的固体动能拦截器助推段最优控制方案研究[J].固体火箭技术,2008,31(6).
作者姓名:潘伟  路长厚  冯维明  葛培琪
作者单位:1. 山东大学机械学院,济南,250061
2. 山东大学,土建学院,济南,250061
基金项目:国家863资助项目  
摘    要:针对三维空间内的高速飞行目标,提出了一种可用于固体动能拦截器助推段的精确最优控制方法。考虑了地球非球形摄动的影响,建立了有限推力拦截器最优控制问题动力学模型,并用直接配置法与SQP方法进行了数值求解,得到了更加精确的助推段控制方案。算例证明该方法有效。

关 键 词:固体动能拦截器  地球非球形摄动  助推段  最优控制

Research on optimal control scheme of solid propellant interceptor in boost phase based on an oblate earth model
PAN Wei,LU Chang-hou,FENG Wei-ming,GE Pei-qi.Research on optimal control scheme of solid propellant interceptor in boost phase based on an oblate earth model[J].Journal of Solid Rocket Technology,2008,31(6).
Authors:PAN Wei  LU Chang-hou  FENG Wei-ming  GE Pei-qi
Institution:PAN Wei1,LU Chang-hou1,FENG Wei-ming2,GE Pei-qi1
Abstract:Aiming at the high speed flight targets in three-dimensional space,an accurate optimal control method for solid propellant interceptor in boost stage was put forward.Considering oblateness of the earth,the kinetics model of optimal control problem of limit thrust interceptor was derived.The problem was solved numerically by means of the direct collocation method and SQP.A more accurate optimal control scheme for the boost stage was obtained.The effectiveness of the method is verified by the example.
Keywords:solid propellant interceptor  earth oblateness  boost phase  optimal control
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