Observability-Based Space Noncooperative Target Motion Estimation

IF 5.7 2区 计算机科学 Q1 ENGINEERING, AEROSPACE IEEE Transactions on Aerospace and Electronic Systems Pub Date : 2024-09-13 DOI:10.1109/TAES.2024.3460756
Yijie Zhang;Jiongqi Wang;Bowen Sun;Bowen Hou;Dayi Wang;Xuanying Zhou
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Abstract

This study proposes a complete method for estimating the relative motion parameters of noncooperative targets in space and analyzes the system observability for the optically autonomous relative navigation problem of noncooperative targets in space. First, using the installation offset of the onboard monocular camera, a relative navigation system model is established herein by observing the three feature points of the target using the line-of-sight direction of the feature points as the measurement information and combining the target's relative orbital dynamics, attitude kinematics, and dynamics. Second, the system observability is analyzed based on the system observability matrix and combined with the null-space theory. The conditions under which the system does not satisfy the observability are analyzed through the definition of observability. An iterative extended Kalman filter based on this system model is then derived to realize the complete estimation of the target relative position, relative velocity, target attitude, angular velocity, inertia ratio, and position of the feature points under the target body frame. Finally, the effect of the camera offset on the system observability is analyzed through a numerical simulation. The results verify that an appropriate camera offset can make the monocular relative navigation system fully observable. The only existing unobservable state variable is found at 0 camera offset.
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基于可观测性的空间非合作目标运动估计
提出了一种完整的空间非合作目标相对运动参数估计方法,分析了空间非合作目标光学自主相对导航问题的系统可观测性。首先,利用机载单目摄像机的安装偏移量,以特征点的视距方向为测量信息,结合目标的相对轨道动力学、姿态运动学和动力学,对目标的三个特征点进行观测,建立相对导航系统模型;其次,基于系统可观测性矩阵,结合零空间理论对系统可观测性进行了分析。通过可观测性的定义,分析了系统不满足可观测性的条件。然后基于该系统模型推导出迭代扩展卡尔曼滤波,实现了目标体框架下目标相对位置、相对速度、目标姿态、角速度、惯性比和特征点位置的完整估计。最后,通过数值模拟分析了摄像机偏移量对系统可观测性的影响。结果表明,适当的相机偏移量可以使单目相对导航系统完全可观测。唯一存在的不可观察状态变量是在0摄像机偏移处找到的。
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来源期刊
CiteScore
7.80
自引率
13.60%
发文量
433
审稿时长
8.7 months
期刊介绍: IEEE Transactions on Aerospace and Electronic Systems focuses on the organization, design, development, integration, and operation of complex systems for space, air, ocean, or ground environment. These systems include, but are not limited to, navigation, avionics, spacecraft, aerospace power, radar, sonar, telemetry, defense, transportation, automated testing, and command and control.
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