Abstract
Based on the non-gyro inertial navigation system, the measurement principle was analyzed, and a kind of nine- accelerometer configuration scheme was designed which is easy to engineering realization. The attitude measurement method of this accelerometer configuration scheme was researched.
| Original language | English |
|---|---|
| Pages (from-to) | 483-485 |
| Number of pages | 3 |
| Journal | Zhongnan Daxue Xuebao (Ziran Kexue Ban)/Journal of Central South University (Science and Technology) |
| Volume | 42 |
| Issue number | SUPPL. 1 |
| Publication status | Published - Sept 2011 |
| Externally published | Yes |
Keywords
- Accelerometer
- Attitude measurement
- GFSINS