TY - JOUR
T1 - How are multiple satellites seen from the ground? Relative apparent motion and formation stabilization
AU - Nakajima, Kenta
AU - Yoshimura, Yasuhiro
AU - Chen, Hongru
AU - Hanada, Toshiya
N1 - Publisher Copyright:
© Tsinghua University Press 2023.
PY - 2024/3
Y1 - 2024/3
N2 - This paper answers how multiple satellites are seen from the ground. This question is inspired by space-advertising, a public exhibition in the night sky using a dot matrix of satellites that are bright enough to be seen by the naked eye. Thus, it is important for space advertisement that the specific dot matrix is seen. Moreover, the stability of the dot matrix during a visible span is very valuable. To stabilize the dot matrix, this study formulates an apparent position of a dot from a representative dot seen from the ground. The formulation, linear functions of a set of relative orbital elements, reveals the appearance of the dot matrix. The proposed relative variable in the formulation drives the instability of the dot matrix, thereby revealing an initial stable configuration of deputies from a chief. The arbitrary dot matrix designed using the configuration is stable even at low elevations without orbital control during the visible span. (Figure presented.)
AB - This paper answers how multiple satellites are seen from the ground. This question is inspired by space-advertising, a public exhibition in the night sky using a dot matrix of satellites that are bright enough to be seen by the naked eye. Thus, it is important for space advertisement that the specific dot matrix is seen. Moreover, the stability of the dot matrix during a visible span is very valuable. To stabilize the dot matrix, this study formulates an apparent position of a dot from a representative dot seen from the ground. The formulation, linear functions of a set of relative orbital elements, reveals the appearance of the dot matrix. The proposed relative variable in the formulation drives the instability of the dot matrix, thereby revealing an initial stable configuration of deputies from a chief. The arbitrary dot matrix designed using the configuration is stable even at low elevations without orbital control during the visible span. (Figure presented.)
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U2 - 10.1007/s42064-023-0180-6
DO - 10.1007/s42064-023-0180-6
M3 - Article
AN - SCOPUS:85187165838
SN - 2522-0098
VL - 8
SP - 121
EP - 134
JO - Astrodynamics
JF - Astrodynamics
IS - 1
ER -