2004年4月
多数機フォーメーションフライトのための連続推力推進による燃料最小誘導則
日本航空宇宙学会論文集
- ,
- ,
- 巻
- 52
- 号
- 601
- 開始ページ
- 72
- 終了ページ
- 79
- 記述言語
- 日本語
- 掲載種別
- 研究論文(学術雑誌)
- DOI
- 10.2322/jjsass.52.72
- 出版者・発行元
- 一般社団法人 日本航空宇宙学会
A continuous-thrust guidance algorithm suitable for a formation flying of a large number of spacecraft having electric propulsion systems are discussed. This algorithm generates continuous-thrust transfer trajectory between any two arbitrary states, which can be optimized in term of total fuel consumption for a formation changing. The algorithms are effective not only in term of fuel consumption but also in term of information quantity to be shared among member spacecraft. Moreover taking computational simplicity into consideration, a quasi-optimal continuous-thrust guidance algorithm are derived.
- リンク情報
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- DOI
- https://doi.org/10.2322/jjsass.52.72
- CiNii Articles
- http://ci.nii.ac.jp/naid/10012050086
- CiNii Books
- http://ci.nii.ac.jp/ncid/AA11307372
- ID情報
-
- DOI : 10.2322/jjsass.52.72
- ISSN : 1344-6460
- CiNii Articles ID : 10012050086
- CiNii Books ID : AA11307372