首页 | 本学科首页   官方微博 | 高级检索  
     检索      

吸气式空天飞行器闭环上升制导研究
引用本文:泮斌峰,唐硕.吸气式空天飞行器闭环上升制导研究[J].飞行力学,2010,28(6).
作者姓名:泮斌峰  唐硕
作者单位:西北工业大学,航天学院,陕西,西安,710072
摘    要:闭环上升制导是吸气式空天飞行器达到快速优化、实时规划以及自主制导的必然要求。采用GHAME吸气式空天飞行器作为研究对象,提出了闭环上升制导最优控制方案,重点论证了该方案不存在关于节流阀值的奇异问题,并阐述了最优推力控制的Bang-Bang控制。引入有限差分法求解两点边值问题,并通过终端时刻调节算法求解终端时刻自由问题。仿真结果表明,所提出的闭环制导算法是有效、可行的,具有显著的优越性。

关 键 词:吸气式空天飞行器  闭环上升制导  最优控制  有限差分法  

Closed-loop ascent guidance of air-breathing aerospace vehicle
PAN Bin-feng,TANG Shuo.Closed-loop ascent guidance of air-breathing aerospace vehicle[J].Flight Dynamics,2010,28(6).
Authors:PAN Bin-feng  TANG Shuo
Institution:PAN Bin-feng,TANG Shuo(College of Astronautics,Northwestern Polytecnical University,Xi'an 710072,China)
Abstract:Closed-loop ascent guidance of the air-breathing aerospace vehicle arises from the requests of rapid optimization,real-time planning and autonomous guidance.This article presents an optimal solution for this problem,taking the GHAME air-breathing aerospace vehicle as a research object.Arguments that there is no singular problem and the thrust follows bang-bang control are given.The finite difference method is introduced to solve two-point boundary value problem,and a final time adjusting algorithm is develo...
Keywords:air-breathing aerospace vehicle  closed-loop ascent guidance  optimal control  finite difference method  
本文献已被 CNKI 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号