Abstract
An accurately linearized in-motion alignment with a large heading error is proposed for a low-cost inertial navigation system with the aiding of global positioning system. The linearization is designed for both the coarse and the fine stages in the local level frame. A criterion is constructed to determine the time to switch the alignment from the coarse stage to the fine one automatically. A vehicle test demonstrates that the proposed alignment converges fast and accurately.
| Original language | English |
|---|---|
| Article number | 8809209 |
| Pages (from-to) | 1917-1925 |
| Number of pages | 9 |
| Journal | IEEE Transactions on Aerospace and Electronic Systems |
| Volume | 56 |
| Issue number | 3 |
| DOIs | |
| State | Published - Jun 2020 |
Keywords
- Global positioning system (GPS)
- Kalman filter (KF)
- inertial navigation system (INS)
- initial alignment
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