摘要
综合考虑卫星外形尺寸、预测时间、初始协方差阵以及空间摄动的影响,提出了一种精确的基于碰撞概率的碰撞检测评估方法。考虑到分布式卫星沿迹向位置误差很难精确预测,本文提出了一种基于判定垂直于沿迹向的平面(X-Z投影面)碰撞概率来进行碰撞规避轨道机动的保守性自主安全运行方法。最后,运用本文提出的碰撞检测评估方法,对影响分布式卫星空间构形被动运行安全性的因素进行了分析,并提出了具有良好被动运行安全性分布式卫星空间构形的设计方法。
In this paper a more precise collision monitoring method is proposed first, which takes the influences of the shape of satellite, predict time, relative covariance matrix and all kinds of perturbations into consideration. Then, because it is very difficult to predict the error of along track position, a conservative autonomous safety operational method based on the judgment of the collision probability in the projected X-Z plane is presented. Finally, the proposed collision monitoring algorithm is used to analyze the passive operational safety of Direct Satellite System (DSS), and a new formation geometry design method is proposed. By using this new design method the DSS can have good passive operational safety.
出处
《吉林大学学报(工学版)》
EI
CAS
CSCD
北大核心
2009年第5期1395-1400,共6页
Journal of Jilin University:Engineering and Technology Edition
基金
教育部创新团队项目(IRT0520)
"十一五"预研背景项目(113020102)
博士后科学基金项目(20070410265)
关键词
飞行器控制和导航技术
分布式卫星系统
碰撞检测
概率密度函数
被动安全性
control and navigation technology of aerospace
distributed satellite system
collision monitoring
probability density function
passive safety