基于多视线融合的高轨近场感知队形设计

doi:10.12305/j.issn.1001-506X.2023.12.29

Abstract

Abstract:

For the problem of near-field situation awareness (NSA) of high orbit satellite, this paper proposes a multi-satellite cooperative NSA scheme based on multi-line-of-sight (LOS) fusion and studies the method of configuration design with the consideration of relative state estimation's accuracy and sunlight constraint. Firstly, based on the system state equation, measurement equation, and extended Kalman filter algorithm, the NSA model with multi-LOS fusion is proposed. Secondly, through theoretical analysis, the configuration optimization criterion that the more the LOS angle approaching 90°, the smaller the target position estimation error is proposed. Thirdly, considering the constraints of sunlight and bounded relative motion, the configuration optimization strategy for NSA is proposed, which is transformed to a nonlinear programming problem solved by the penalty function method. Finally, numerical simulations are conducted to validate the effectiveness of the proposed multi-LOS fusion NSA model, configuration optimization design criterion, and configuration optimization strategy of NSA.

Key words: multi-spacecraft, angle-only, near-field situation awareness (NSA), configuration design, non-cooperative target

CLC Number:

V448.2

Dawei FAN, Weiwei CAI, Leping YANG, Runde ZHANG. Multi-line-of-sight fusion based configuration design for near-field situation awareness in high orbit[J]. Systems Engineering and Electronics, 2023, 45(12): 3984-3994.

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References 25

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轨道根数	主星	从星1	从星2	目标
a/m	42 164 169	42 164 169	42 164 169	42 154 169
e	0	0.000 4	0.000 2	0.000 3
I/(°)	50	50.5	49.9	50.3
Ω/(°)	10	10.5	9.95	10
ω/(°)	20	20.05	20.05	20.3
M/(°)	6	6.045 2	5.997 6	5.946 4

轨道根数	主星	从星1	从星2	目标1
a/m	42 164 169	42 164 169	42 164 169	42 114 169
e	0	0.001 27	0	0
I/(°)	5	5.013 6	4.986 5	5
Ω/(°)	10	10	9.983 8	10
ω/(°)	20	40	0	20
M/(°)	6	-14	26	6

轨道根数	主星	从星1	从星2	目标2
a/m	42 164 169	42 164 169	42 164 169	42 164 169
e	0	0.006 79	0.005 91	0.001
I/(°)	5	5.013 6	4.986 4	5.5
Ω/(°)	10	10	10	10
ω/(°)	20	40	0	20
M/(°)	6	-14	26	6

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Multi-line-of-sight fusion based configuration design for near-field situation awareness in high orbit

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