Optimal direct ascent to GEO using laser propulsion system
碩士 === 國立中央大學 === 機械工程研究所 === 82 === The optimal trajectory for direct ascent to the geosynchronous earth orbit (GEO) with prescribed longitudinal displacement will be solved by using parameter optimization method. The time derivative of th...
| Main Authors: | , |
|---|---|
| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
1994
|
| Online Access: | http://ndltd.ncl.edu.tw/handle/47327631886770076419 |