TY - JOUR
T1 - Orbital Configuration Control for Space-based Gravitational Wave Observatory Based on the Output Regulation Theory
AU - Pan, Zhengxu
AU - Bando, Mai
AU - Zhu, Zhanxia
AU - Hokamoto, Shinji
N1 - Publisher Copyright:
Copyright © 2025 The authors.
PY - 2025
Y1 - 2025
N2 - This paper presents an analysis of the formation of an equilateral triangle for a space-based gravitational wave observatory (GWO) near a collinear libration point in the circular-restricted three-body problem. To achieve continuous observation of gravitational waves, stable triangle configurations are required. However, the motion near the collinear libration points is highly unstable. This problem is examined by employing a two-layer design. In an inner-layer loop, the tracking problem is solved by using the output regulation theory to establish equilateral triangle formation in two periods. As for the outer-layer loop, the radius, frequency, and direction angle of the formation are examined. These parameters play a crucial role in establishing a stable and efficient triangle formation configuration for the GWO. Finally, when the radius, frequency and direction angle are changed, the fuel consumption that required to initialize and maintain the desired formation is calculated.
AB - This paper presents an analysis of the formation of an equilateral triangle for a space-based gravitational wave observatory (GWO) near a collinear libration point in the circular-restricted three-body problem. To achieve continuous observation of gravitational waves, stable triangle configurations are required. However, the motion near the collinear libration points is highly unstable. This problem is examined by employing a two-layer design. In an inner-layer loop, the tracking problem is solved by using the output regulation theory to establish equilateral triangle formation in two periods. As for the outer-layer loop, the radius, frequency, and direction angle of the formation are examined. These parameters play a crucial role in establishing a stable and efficient triangle formation configuration for the GWO. Finally, when the radius, frequency and direction angle are changed, the fuel consumption that required to initialize and maintain the desired formation is calculated.
KW - Circular-restricted Three-body Problem
KW - Gravitational Wave Observatory
KW - Output Regulation Theory
KW - Two-layer Design
UR - http://www.scopus.com/inward/record.url?scp=86000140225&partnerID=8YFLogxK
U2 - 10.2322/tjsass.68.98
DO - 10.2322/tjsass.68.98
M3 - 文章
AN - SCOPUS:86000140225
SN - 0549-3811
VL - 68
SP - 98
EP - 107
JO - Transactions of the Japan Society for Aeronautical and Space Sciences
JF - Transactions of the Japan Society for Aeronautical and Space Sciences
IS - 2
ER -