文件名称:GA_missile_trajectory_simulation
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提出了一种空面导弹下滑段、俯冲攻击段的弹道优化设计方案,以及一
种实现航向动态跟踪的具体方法。大量算例表明,采用本文中的空面导弹控制
方案可以设计、调试出较满意的弹道,达到获取导弹飞行性能数据并验证导弹总
体设计参数的目的。
-A decline in air-surface missile paragraph, paragraph ballistic dive attack to optimize the design of programs, as well as a course to achieve dynamic tracking of specific methods. A large number of examples show that the use of space in this article surface missile control program can design, debug a more satisfactory trajectory to obtain the missile flight performance data and verify the purpose of missile design parameters.
种实现航向动态跟踪的具体方法。大量算例表明,采用本文中的空面导弹控制
方案可以设计、调试出较满意的弹道,达到获取导弹飞行性能数据并验证导弹总
体设计参数的目的。
-A decline in air-surface missile paragraph, paragraph ballistic dive attack to optimize the design of programs, as well as a course to achieve dynamic tracking of specific methods. A large number of examples show that the use of space in this article surface missile control program can design, debug a more satisfactory trajectory to obtain the missile flight performance data and verify the purpose of missile design parameters.
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空面导弹弹道仿真方法研究.caj