A basic study about the optimal orbit control of a DAS
| Autor: | Fu, Tianshuang, Imado, Fumiaki |
|---|---|
| Jazyk: | angličtina |
| Rok vydání: | 2006 |
| Předmět: |
最急上昇法
numerical analysis optimal trajectory orbit determination Computer Science::Neural and Evolutionary Computation 高度 steepest ascent method 最適制御 optimal control orbit calculation 軌道決定 軌道制御 超低高度衛星 trajectory control 数値解析 DAS 衛星軌道 最適軌道 satellite orbit 数学モデル perigee dive and ascent satellite 軌道計算 近地点 mathematical model altitude |
| Zdroj: | 第15回アストロダイナミクスシンポジウム講演後刷り集 2005 = Proceedings of 15th Workshop on JAXA Astrodynamics and Flight Mechanics. :395-400 |
| Popis: | A study about the optimal orbit control of a Dive and Ascent Satellite (DAS) is presented. The DAS is a satellite that can dive close to the earth, and get detailed information we need. The optimal orbit control problems are reduced to nonlinear two-point boundary value problems. In this paper we solve them by using the steepest ascent method for minimum fuel consumption 資料番号: AA0063480061 |
| Databáze: | OpenAIRE |
| Externí odkaz: |
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