Preliminary Study on Control of Satellite Formation Flying Around L2 Using Solar Sail Propulsion

Triwanto Simanjuntak; Mutsuko Y. Morimoto; Sawada Hirotaka; Yuichi Tsuda; Junichiro Kawaguchi

doi:10.11511/jacc.50.0.104.0

Proceedings of the 50th Japan Joint Automatic Control Conference

セッションID: 328

DOI https://doi.org/10.11511/jacc.50.0.104.0

会議情報

主催: The Japan Society of Mechanical Engineers, The Society of Instrument and Control Engineers, The Institute of Systems, Control and Information Engineers, The Society of Chemical Engineers, Japan, The Japan Society for Precision Engineering, The Japan Society for Aeronautical and Space Sciences

共催: Technically Cosponsored by 42 Societies and Institutes

ＯＳ１９　航空宇宙における誘導制御（_II_）

Preliminary Study on Control of Satellite Formation Flying Around L2 Using Solar Sail Propulsion

*Triwanto Simanjuntak, Mutsuko Y. Morimoto, Sawada Hirotaka, Yuichi Tsuda, Junichiro Kawaguchi

著者情報

キーワード: Formation Fyling Control, Lagrangian Libration Point, Solar Sail Propulsion, Restricted Three Body Problem

会議録・要旨集フリー

詳細

抄録

Lagrangian libration point, L2 offers strategic location for astronomical observations. Here at L2, introduced a satellite formation flying consists of two satellites powered by solar sail, the Mirror Spacecraft (MSC) and the Detector Spacecraft (DSC). The two satellites are separated such that the operational detector is at the focus of the mirror. Due to the instability of the collinear Lagrangian points, the desired distance between the two satellites need to be maintained. This paper addresses the control design scheme for station keeping control. The equation of motion is derived in Hill's frame and inertial frame and then control law formulated mathematically. Halo and Lissajous orbit are considered as options for reference orbit.

責任著者(Corresponding author)

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