On the Satellite Attitude Determination by Using the Optimal Estimation Method
碩士 === 逢甲大學 === 航太與系統工程所 === 95 === The attitude of a satellite defines its orientation in inertial space. Knowledge of the attitude of a satellite is greatly important for the attitude control. However, the major problem is how to obtain an accurate attitude from the measurement data with imperfect...
| Main Authors: | , |
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| Format: | Others |
| Language: | zh-TW |
| Published: |
2007
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| Online Access: | http://ndltd.ncl.edu.tw/handle/68832460022728692038 |