基于相对角动量的空间非合作目标机动仅测角检测方法

doi:10.12305/j.issn.1001-506X.2023.03.23

Abstract

Abstract:

To improve the performance of maneuver detection for space non-cooperative targets with mall pulse orbit based on existed approaches, an orbit maneuver detection algorithm using angle-only measurements by passive optical camera is developed, where the relative angular momentum is introduced as a new characteristic to be measured. Firstly, the relative dynamics model based on Clohessy-Wiltshire equations and the relative line-of-sight measurement model when the camera is installed off the center of mass are established in the orbit coordinate system. Then, the definition of relative angular momentum is given and the benefit of this characteristic as the test parameter to detect maneuver is analyzed quantitatively. Next, the framework of the maneuver detection algorithm based on variance ratio of double sliding window is designed. Finally, simulations are conducted to verify the effectiveness and performance of the proposed algorithm. The simulation results show that the proposed algorithm can realize the fast orbit maneuver detection to the near-circular orbit target and the error is within 60 s.

Key words: space non-cooperative target, orbital maneuver detection, relative angular momentum, angle-only measurement

CLC Number:

V488.2

Baichun GONG, Xin JIN, Renyong ZHANG, Xiuqiao CHEN. Angle-only measurement maneuver detecting method for space non-cooperative target based on relative angular momentum[J]. Systems Engineering and Electronics, 2023, 45(3): 814-821.

Figures/Tables 11

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References 23

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相对轨道	初始相对位置/m			初始相对速度/(m/s)
相对轨道	X	Y	Z	X	Y	Z
V-bar静止	1 000	0	0	0	0	0
共椭圆飞越	1 000	0	0	0	0	0.563 42
椭圆绕飞	1 000	0	-100	-0.169 26	0	0
面外振荡	1 000	0	0	0	-0.112 84	0

测角均方差/rad	ΔV=0.950~1.000 m/s		ΔV=0.095~0.100 m/s
测角均方差/rad	检测误差＜60 s	检测误差＜120 s	检测误差＜60 s	检测误差＜120 s
3×10^-5	95.6	98.3	93.7	96.3
3×10^-4	99.3	100.0	97.3	98.0
3×10^-3	99.0	99.5	78.7	82.0

相对轨道	机动方向	ΔV=0.1 m/s时的误差/s	ΔV=1 m/s时的误差/s	相对轨道	机动方向	ΔV=0.1 m/s时的误差/s	ΔV=1 m/s时的误差/s
V-bar静止	X	3.63	27.64	共椭圆飞越	X	24.31	44.45
	Z	48.52	54.45		Z	48.30	52.70
	Y	46.26	28.38		Y	12.19	37.15
椭圆绕飞	X	46.29	53.05	面外振荡	X	13.67	32.15
	Z	49.80	55.32		Z	39.47	51.70
	Y	43.79	51.45		Y	34.00	46.13

Angle-only measurement maneuver detecting method for space non-cooperative target based on relative angular momentum

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