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高超声速无动力滑翔三维轨迹规划方法
引用本文:闫晓东,王智.高超声速无动力滑翔三维轨迹规划方法[J].北京理工大学学报,2013,33(7):669-674.
作者姓名:闫晓东  王智
作者单位:西北工业大学航天学院,陕西,西安 710072;航天飞行动力学技术重点实验室,北京 100094;西北工业大学航天学院,陕西,西安 710072
基金项目:国家教育部高校学报博士学科点新教师基金资助项目(20116102120004)
摘    要:轨迹规划是进行高超声速滑翔飞行器任务设计以及提高制导方法适应性的有效途径. 定义了目标平面坐标系,并将该坐标系作为参考坐标系推导了归一化能态方程. 该方程具有定积分区间的优点,并可用状态直接表征横程和纵程. 基于该方程提出了纵向轨迹规划方法和侧向轨迹规划方法,并考虑轨迹横向曲率,提出了结合纵向轨迹规划方法和侧向轨迹规划方法的三维轨迹规划方法. 仿真计算结果表明该方法可快速、精确地完成高超声速滑翔飞行器的滑翔轨迹规划. 

关 键 词:高超声速滑翔飞行器  轨迹规划  动力学方程  制导
收稿时间:6/8/2012 12:00:00 AM

Three-Dimensional Trajectory Planning Method for Hypersonic Glide Vehicles
YAN Xiao-dong and WANG Zhi.Three-Dimensional Trajectory Planning Method for Hypersonic Glide Vehicles[J].Journal of Beijing Institute of Technology(Natural Science Edition),2013,33(7):669-674.
Authors:YAN Xiao-dong and WANG Zhi
Institution:1.College of Astronautics, Northwestern Polytecnical University, Xi'an, Shaanxi 710072, China;National Key Laboratory of Aerospace Flight Dynamics, Beijing 100094, China2.College of Astronautics, Northwestern Polytecnical University, Xi'an, Shaanxi 710072, China;
Abstract:It's an effective way to improve the guidance adaptability for hypersonic glide vehicle (HGV) by applying trajectory planning. First, the target plane coordinate frame was defined. Then, taking the coordinate frame as the reference coordinate frame, dynamic equations with the normalized energy as independent variable were deduced, which have the advantages of fixed integral interval, and cross-range and longitudinal range could be denoted by the equation states. Based on the equations, longitudinal trajectory planning method was put forward as well as lateral trajectory planning method. With the combination of above methods and the trajectory of lateral curvature, a three-dimensional trajectory planning method has been implemented. It is shown that the proposed method can fulfill trajectory planning for HGV rapidly and accurately.
Keywords:hypersonic glide vehicles  trajectory planning  dynamics equation  guidance
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