基于解析法最优轨迹的在线实时制导律研究 |
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引用本文: | 张志国,余梦伦.基于解析法最优轨迹的在线实时制导律研究[J].导弹与航天运载技术,2016(5):58-61. |
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作者姓名: | 张志国 余梦伦 |
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作者单位: | 北京宇航系统工程研究所,北京,100076 |
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摘 要: | 新型制导系统单纯采用轨迹优化的数值算法的优点是精度高,但耗时长,算法稳定性有待提高,随着计算机技术的发展,耗时长的缺点能得到缓解,但仍然无法满足实时动态制导控制需求。数值法以前,解析法曾得到深入的研究,如果能结合二者的优点,将能更好地达到提升飞行器实时高精度制导控制的效果。用解析法求解了轨迹优化问题中的两点边值问题,并和数值打靶法对比分析了入轨精度和计算时间的差异,得出各自方法的优缺点。
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关 键 词: | 实时在线制导 解析法 轨迹优化 |
Online Real-time Guidance Law Using an Analytical Optimal-trajectory Method |
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Abstract: | The numerical guidance methods of optimal trajectory are high accuracy, but time-consuming and algorithm-unstable. With the development of computer technology, time-consuming weakness can be alleviated, but still unable to meet the real-time dynamic guidance and control requirements. Analytical methods have been in-depth study before the instance of numerical methods. If combines the advantages of these two methods, it will be able to achieve the real-time control with high accuracy. Firstly, an analytical method is solved with the two-point boundary-value problem of optimal trajectory, then analyze the differences of in-orbit precision and computing time between the analytical and numerical methods. Finally, the advantages and disadvantages of each method are given. |
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Keywords: | Online real-time guidance Analytical method Trajectory optimization |
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