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A parametric design method of nanosatellite close-range formation for on-orbit target inspection

This paper proposes an efficient design method for nano satellites formation flying near a large space target to perform ultra-close inspection missions. A parametric model for periodic relative motion between two satellites is firstly proposed through a detailed analysis of the relative orbital dyn...

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Published in:Chinese journal of aeronautics 2023-10, Vol.36 (10), p.194-209
Main Authors: JIAO, Bohan, SUN, Qinbo, HAN, Hongyu, DANG, Zhaohui
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Language:English
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cited_by cdi_FETCH-LOGICAL-c372t-be4a47b30b46a1be2f0e5ec644fa64d066c4e8d7cb505517375e6e3171d98ed93
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container_end_page 209
container_issue 10
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container_title Chinese journal of aeronautics
container_volume 36
creator JIAO, Bohan
SUN, Qinbo
HAN, Hongyu
DANG, Zhaohui
description This paper proposes an efficient design method for nano satellites formation flying near a large space target to perform ultra-close inspection missions. A parametric model for periodic relative motion between two satellites is firstly proposed through a detailed analysis of the relative orbital dynamics. It is proved that the existing periodic solutions of satellite relative motion such as in-plane 2:1 elliptic and circular periodic relative orbits both belong to the ellipsoid family of periodic relative orbits. The motion planes and their locations and orientations of the general periodic relative orbits are then determined as the analytic functions of the initial relative states. The maximal and minimal distances from the relative orbit to the origin are further analytically calculated too. A formation design algorithm is then proposed for optimal observation of feature points of the target considering various requirements of collision avoidance and observable distance by using this parametric model. Numerical examples about target inspection are introduced to quantitively evaluate and verify the models and methods. The simulation results are well consistent with the theoretical predictions, showing that the design proposed can be potentially applied for future practical on-orbit service missions.
doi_str_mv 10.1016/j.cja.2023.06.003
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ispartof Chinese journal of aeronautics, 2023-10, Vol.36 (10), p.194-209
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subjects Ellipsoid family
Formation flying
Nanosatellite
Periodic relative orbit
Target tracking and inspection
title A parametric design method of nanosatellite close-range formation for on-orbit target inspection
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