碩士 / 中原大學 / 電機工程研究所 / 92 / Using the data fusion of GPS and INS signals, an integrated system based on Kalman
lter is proposed to estimate the navigation information. Kalman lter has many di erent
forms. In order to cooperate the indirect Kalman lter, we rst establish the error state
equations of inertial navigation system. Then feedforward and feedback indirect Kalman
lters are used to estimate the error states, which in turn correct the navigation states
to prevent the divergence due to measurement error. In simulation, the
ying course of
an aircraft from C.K.S. airport to Nagoya airport is considered to verify the purposed
method.
| Identifer | oai:union.ndltd.org:TW/092CYCU5442070 |
| Date | January 2004 |
| Creators | Ching-Fu Chang, 張景富 |
| Contributors | Kuang-Yow Lian, 練光祐 |
| Source Sets | National Digital Library of Theses and Dissertations in Taiwan |
| Language | en_US |
| Detected Language | English |
| Type | 學位論文 ; thesis |
| Format | 68 |
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