Spacecraft Attitude Determination by Kalman Filter
碩士 === 國立臺灣大學 === 機械工程研究所 === 82 === The object of this research is to study spacecraft attitude determination by Kalman filter. At first,Kalman filter algorithm is derived and divergence problom also discussed. Next, list the equation of motion of a rigi...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
1994
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| Online Access: | http://ndltd.ncl.edu.tw/handle/32020321508876230023 |