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: | Shen-Tai Lu, 盧申泰 |
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Other Authors: | D. L. Sheu |
Format: | Others |
Language: | zh-TW |
Published: |
2005
|
Online Access: | http://ndltd.ncl.edu.tw/handle/95300863919544711638 |
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