Mixed guidance method for reentry vehicles based on optimization
-
摘要: 在深入研究机动再入飞行器标准轨道和预测制导方法的基础上,针对标准轨道和预测制导相结合的制导方法,分析了由预测制导指令延迟引起的误差,提出了误差补偿策略.根据最优化理论,设计了相关性能指标函数,提出新的预测制导算法.并结合标准轨道法,通过对有限几个特征点位置上引入预测制导,形成了一种基于最优化问题的混合制导方法.有效减小了预测制导指令的解算时间,进一步降低了落点误差.仿真结果表明,该方法既具有较强的抗干扰能力和较高的制导精度,又具有一定的工程实用价值.Abstract: The error caused by the calculating time delay of predictive guidance was analyzed for the mixed guidance based on the reference-trajectory guidance and predictive guidance for reentry vehicles. The method of error compensation was put forward. By utilizing the optimization theory, performance index function was designed and a new predictive guidance method was proposed. The reference-trajectory guidance was combined with predictive guidance which was applied in some characteristic position in the reentry process. A mixed guidance method based on the optimization for the reentry vehicles was proposed, which decreased calculating time of predictive guidance to a satisfactory level and reduced deviation and disturbance further. The simulation results indicate the strong antiinterference capacity, high guidance precision and great practical value in engineering of this method.
-
Key words:
- reentry vehicles /
- reentry guidance /
- optimization /
- predictive guidance
点击查看大图
计量
- 文章访问数: 4206
- HTML全文浏览量: 38
- PDF下载量: 1239
- 被引次数: 0