The Maximum Reachable Domain for a Rocket Flying Over a Rotating Spherical Earth
碩士 === 國立成功大學 === 航空太空工程學系碩博士班 === 93 === In this thesis, the maximum reachable domain for a rocket flying over a spherical earth surface is analyzed by using the optimal control theory. The rocket is assumed to be a point mass. The direction of rocket is controlled by the angle between the thrust...
| Main Authors: | , |
|---|---|
| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2005
|
| Online Access: | http://ndltd.ncl.edu.tw/handle/95300863919544711638 |