連続作動推力の衛星群における離心率分離へのポテンシャル関数誘導法

概要

論文の詳細を見る
The potential-function guidance is applied to the autonomous formation-keeping of the eccentricity separation in the co-located many-satellite system. The acceleration resulting from the continuous and throttled thrust is formulated as a function of positions and velocities of all satellites. If these state variables are measured by on-board sensors, the maneuvering schedule can be computed in the respective satellites. A numerical simulation affirms the validity of the control.
社団法人日本航空宇宙学会の論文
2001-12-05