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

多曝光星敏感器的全运动参数建模及优化设计
引用本文:于文波,武佩,宣传忠,张春慧,江洁.多曝光星敏感器的全运动参数建模及优化设计[J].北京航空航天大学学报,2021,47(10):2006-2012.
作者姓名:于文波  武佩  宣传忠  张春慧  江洁
作者单位:1.内蒙古农业大学 机电工程学院, 呼和浩特 010018
基金项目:内蒙古农业大学高层次人才引进科研启动项目NDYB2018-16国家自然科学基金62005135国家自然科学基金61725501
摘    要:多曝光成像方法是一种有效提升星敏感器姿态更新率的技术,但该方法随着运动角速度及角加速度增大,相邻星点轨迹的交叉概率显著增大,严重影响其提升性能。为了解决上述问题,建立了基于星敏感器全运动参数的星点成像位置模型,并据此确定了星点在工作周期内的运动位移。根据该模型,对交叉概率与全运动参数、焦距、星点位置等的关系进行了仿真,并确定了全运动参数的极限安全值为角速度ω≤26.4(°)/s,角加速度α≤5(°)/s2。外场观星实验充分验证了所提方法的有效性。 

关 键 词:多曝光星敏感器    全运动参数建模    优化设计    仿真分析    外场实验
收稿时间:2020-07-28

Complete motion parameters modeling and optimization design of multiexposure star tracker
YU Wenbo,WU Pei,XUAN Chuanzhong,ZHANG Chunhui,JIANG Jie.Complete motion parameters modeling and optimization design of multiexposure star tracker[J].Journal of Beijing University of Aeronautics and Astronautics,2021,47(10):2006-2012.
Authors:YU Wenbo  WU Pei  XUAN Chuanzhong  ZHANG Chunhui  JIANG Jie
Institution:1.College of Mechanical and Electrical Engineering, Inner Mongolia Agricultural University, Hohhot 010018, China2.School of Instrumentation and Optoelectronic Engineering, Beihang University, Beijing 100083, China
Abstract:The multiexposure imaging method can be utilized to improve the attitude update rate of the star tracker effectively. However, with the increase of the angular velocity and angular acceleration, the cross probability of adjacent star tracks increases significantly, thus seriously affecting the performance of multiexposure imaging method. In order to solve the above problem, first, the star imaging position model based on the complete motion parameters of star tracker is established, and the movement displacement of the star point in the working period is determined accordingly. Then, according to the above model, the relationship between the cross probability and the parameters such as complete motion parameters, focal length and star position, is simulated quantitatively, and the limit safety values of complete motion parameters are determined as angular velocity ω ≤ 26.4(°)/s and angular acceleration α ≤ 5(°)/s2. Finally, a star observation field experiment is carried out to further verify the effectiveness of the proposed method. 
Keywords:
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《北京航空航天大学学报》浏览原始摘要信息
点击此处可从《北京航空航天大学学报》下载免费的PDF全文
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