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高超声速机动目标天基跟踪鲁棒性滤波方法 被引量:1
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作者 魏世君 翟光 +2 位作者 孙一勇 毕幸子 汪宏昇 《宇航学报》 EI CAS CSCD 北大核心 2022年第9期1246-1256,共11页
为解决高超声速滑翔飞行器(HGV)机动飞行过程中的跟踪问题,提出了一种基于机动观测器补偿的鲁棒扩展卡尔曼滤波方法。针对传统卡尔曼滤波器由于模型误差而无法稳定跟踪的问题,首先建立了HGV动力学模型和天基红外测量模型;随后,设计机动... 为解决高超声速滑翔飞行器(HGV)机动飞行过程中的跟踪问题,提出了一种基于机动观测器补偿的鲁棒扩展卡尔曼滤波方法。针对传统卡尔曼滤波器由于模型误差而无法稳定跟踪的问题,首先建立了HGV动力学模型和天基红外测量模型;随后,设计机动观测器对未知气动加速度进行在线估计;在此基础上,利用机动估计对扩展卡尔曼滤波中的预测步骤进行修正,克服了因模型误差而导致的滤波发散问题;最后,考虑到机动观测器的时延误差,在扩展卡尔曼滤波迭代过程中引入次优渐消因子,提高了滤波跟踪的鲁棒性。与强跟踪滤波、扩维卡尔曼滤波、交互多模型滤波等典型跟踪方法相比,所提方法可在不具备目标机动先验信息的情况下,以较低的计算耗时取得良好的稳定性和跟踪精度。 展开更多
关键词 高超声速滑翔飞行器 机动目标跟踪 状态估计 机动观测器 卡尔曼滤波
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Space advanced technology demonstration satellite 被引量:1
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作者 ZHANG XiaoFeng CHEN Wen +66 位作者 ZHU XiaoCheng MENG Na HE JunWang bi xingzi ZHANG YongHe SHI Qi LI Fei LIU Rui FENG ZhengGong LIU Liu LI JinSong WU HaiChen XU DongXiao LI TaiJie HUANG JiangJiang LIU Shuo LI TianTong YU XianSheng GAO Yang ZHOU Heng BAN HanYu ZHANG YanLi ZHANG YueTing YANG YingQuan HE Tao DUAN XuLiang CHEN Xin WANG YaMin SUN AnTai ZHANG KuoXiang SUN Ying WANG Yaobin FAN ChengCheng XIONG ShaoLin LI XinQiao WEN XiangYang LING ZhiXing SUN XiaoJin ZHANG Chen BAI XianYong WANG ZhanShan DENG YuanYong TIAN Hui YANG JianFeng XUE HongBo SANG Peng LIU JinGuo ZHENG HuiLong ZHU Xiang HE JianWu LI Hui XU LuXiang XU ShuYan CHEN WenWu LIU ZhenDong WANG ZhaoLi MAO XiangLong GAO Rong LI ZongXuan DING GuoPeng WANG XinYu DOU RunJiang WENG Lubin LUO Hao WANG YaPing LIANG XianFeng FANG ZiRuo 《Science China(Technological Sciences)》 SCIE EI CAS CSCD 2024年第1期240-258,共19页
The Space Advanced Technology demonstration satellite(SATech-01),a mission for low-cost space science and new technology experiments,organized by Chinese Academy of Sciences(CAS),was successfully launched into a Sun-s... The Space Advanced Technology demonstration satellite(SATech-01),a mission for low-cost space science and new technology experiments,organized by Chinese Academy of Sciences(CAS),was successfully launched into a Sun-synchronous orbit at an altitude of~500 km on July 27,2022,from the Jiuquan Satellite Launch Centre.Serving as an experimental platform for space science exploration and the demonstration of advanced common technologies in orbit,SATech-01 is equipped with 16 experimental payloads,including the solar upper transition region imager(SUTRI),the lobster eye imager for astronomy(LEIA),the high energy burst searcher(HEBS),and a High Precision Magnetic Field Measurement System based on a CPT Magnetometer(CPT).It also incorporates an imager with freeform optics,an integrated thermal imaging sensor,and a multi-functional integrated imager,etc.This paper provides an overview of SATech-01,including a technical description of the satellite and its scientific payloads,along with their on-orbit performance. 展开更多
关键词 SATech-01 spacecraft design scientific instruments on-orbit performance
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