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可重复使用飞行器导航制导控制技术展望
引用本文:王国庆,郭建国,周军,张月玲.可重复使用飞行器导航制导控制技术展望[J].导航与控制,2017,16(5):86-90.
作者姓名:王国庆  郭建国  周军  张月玲
作者单位:1. 西北工业大学精确制导与控制研究所,西安,710072;2. 中国运载火箭技术研究院研发中心,北京,100076
摘    要:针对当前可重复使用飞行器的发展现状,总结了其特点、优势和发展趋势.通过飞行任务,分析了可重复使用飞行器所面临的复杂环境特性和飞行控制特性.从飞行控制角度出发,概括了可重复使用飞行器导航制导控制所面临的技术挑战,包括高精度导航技术、多约束航迹优化技术、再入段和能量管理段的制导技术以及强耦合强不确定强鲁棒姿态控制技术等.最后,针对技术挑战,对可重复使用飞行器导航制导控制技术提出了若干建议.

关 键 词:可重复使用飞行器  导航  制导控制  轨迹优化

Prospects for Navigation, Guidance and Control Technology of Reused Launch Vehicle
WANG Guo-qing,GUO Jian-guo,ZHOU Jun and ZHANG Yue-ling.Prospects for Navigation, Guidance and Control Technology of Reused Launch Vehicle[J].Navigation and Control,2017,16(5):86-90.
Authors:WANG Guo-qing  GUO Jian-guo  ZHOU Jun and ZHANG Yue-ling
Institution:Institute of Precision Guidance and Control,Northwestern Polytechnical University,Xi''an 710072,Institute of Precision Guidance and Control,Northwestern Polytechnical University,Xi''an 710072,Institute of Precision Guidance and Control,Northwestern Polytechnical University,Xi''an 710072 and China Academy of Launch Vehicle Technology,Beijing 100076
Abstract:The feather,advantage and tendency of reused launch vehicle are summarized according to the state of arts of vehicle.The complicated environment characteristics and flight control properties are analyzed according to flight mission.Furthermore,the challenges in navigation,guidance and control technology for reused launch vehicle in the view of flight control are presented including navigation technology with high precision,trajectory optimization technology with multi-constraints,guidance technology in the reentry phase and energy management,and robust coupling attitude control technology under strong uncertainties.Finally,some key issues are proposed for navigation,guidance and control of reused launch vehicle on the basis of the challenges.
Keywords:reusable launch vehicle  navigation  guidance and control  trajectory optimization
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