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基于多分辨率技术的滑翔飞行器轨迹优化算法
引用本文:陈小庆,侯中喜,刘建霞. 基于多分辨率技术的滑翔飞行器轨迹优化算法[J]. 宇航学报, 2010, 31(8). DOI: 10.3873/j.issn.1000-1328.2010.08.000
作者姓名:陈小庆  侯中喜  刘建霞
作者单位:国防科技大学航天与材料工程学院,长沙,410073
基金项目:国家自然科学基金,湖南省优秀研究生创新基金 
摘    要:针对滑翔飞行器轨迹优化展开研究。采用了考虑地球扁率和自转的动力学模型,大气模型采用较精确的大气模型。滑翔式飞行器轨迹优化具有强非线性和多约束等特点,为克服传统优化方法对初始值较敏感且难以处理航路点等状态约束,同时在精度和计算速度之间取得一定的平衡,提出采用基于网格自适应的多分辨率技术对滑翔飞行器轨迹进行优化,并对航路点约束提出了相应的处理策略。针对包含航路点、禁飞区和终端约束的典型工程问题展开了轨迹优化研究。仿真实验表明,一条行程12400 km的滑翔弹道优化耗时约200 s,验证了该算法的有效性,对工程实践具有一定的参考意义。

关 键 词:滑翔飞行器  轨迹优化  多分辨率技术

A Multiresolution Technique-Based Gliding Vehicle Trajectory Optimization Algorithm
CHEN Xiao-qing,HOU Zhong-xi,LIU Jian-xia. A Multiresolution Technique-Based Gliding Vehicle Trajectory Optimization Algorithm[J]. Journal of Astronautics, 2010, 31(8). DOI: 10.3873/j.issn.1000-1328.2010.08.000
Authors:CHEN Xiao-qing  HOU Zhong-xi  LIU Jian-xia
Affiliation:CHEN Xiao-qing,HOU Zhong-xi,LIU Jian-xia(College of Aerospace and Materials Engineering,National University of Defense Technology,Changsha 410073,China)
Abstract:The trajectory optimization problem of a gliding vehicle ia researched in this paper.A dynamics model including the Earth rotation and the J2 term perturbation is used to optimize the design,and the accurate atmospheric model is adopted.In the light of the strong nonlinearity and various constraint characteristics of trajectory optimization,traditional trajectory optimization technique is sensitive to the initial guess and it is hard to deal with constraints such as way point and so on;based on a simple and...
Keywords:Gliding vehicle  Trajectory optimization  Multiresolution technique  
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