日本航空宇宙学会論文集
Online ISSN : 2432-3691
Print ISSN : 1344-6460
ISSN-L : 1344-6460
論文
エレクトロダイナミックテザー推進における電流入力整形
渡部 武夫藤井 裕矩小島 広久William Singhose
著者情報
ジャーナル フリー

2005 年 53 巻 623 号 p. 569-576

詳細
抄録
This paper discusses an Input Shaping method for electrodynamic tether systems. The Input Shaping method is applied to generate an input current profile to reduce the induced vibration of the electrodynamic tether system in the initial phase of the propulsion. The Lorenz force and the flexibility of the tether cause vibrations of the tether system on orbit. Two different shapers are designed to suppress the two main vibration modes. The complete shaper is designed by multiplying each of the shapers together. The flexibility of the tether is described by the lumped mass model. The robustness of the shapers is discussed by sensitivity plots. The results of numerical simulations show excellent performance of vibration suppressing by the employing Input Shaping for the electrodynamic tether system.
著者関連情報
© 2005 The Japan Society for Aeronautical and Space Sciences
前の記事 次の記事
feedback
Top