摘要
为了提高对空间目标的拦截成功率,可采用拦截器从停泊轨道转移进入拦截轨道逆轨网捕拦截的方式。利用椭圆弹道理论,讨论和分析了该拦截方式停泊轨道优化问题的描述、模型的建立及优化的方法。计算结果表明,对该拦截方式所建立的模型和采用的优化方法满足逆轨拦截对轨道设计的要求,可为空间快速拦截应用提供理论借鉴和参考。
To improve the success rate of interception for space target,the reverse interception method can be adopted for interceptor by transferring from berthing orbit to interception orbit. By using the elliptic trajectory theory,the paper describes and analyzes the description of the optimization issue of the berthing orbit,the model establishment and the optimization method. The calculation results show that the designed berthing orbit which is got by the optimal model and method can satisfy the requirement of track design for reverse orbit interception. This achievement can provide theoretical reference for rapid space interception applications.
作者
魏鹏涛
WEI Peng-tao(Command Department, Rocket Force Command College, Wuhan 430012, China)
出处
《飞行力学》
CSCD
北大核心
2017年第6期61-64,69,共5页
Flight Dynamics
关键词
空间目标
网捕拦截
停泊轨道优化
遗传算法
space target
rope net interception
berthing orbit optimal
genetic algorithm
