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: | , |
---|---|
Other Authors: | |
Format: | Others |
Language: | zh-TW |
Published: |
2007
|
Online Access: | http://ndltd.ncl.edu.tw/handle/68832460022728692038 |