- Category:
- matlab
- Tags:
-
- File Size:
- 1kb
- Update:
- 2017-11-20
- Downloads:
- 1 Times
- Uploaded by:
- 刘柳
Description: A linear constant acceleration rocket flight in the air along the acceleration, the engine thrust fluctuation will cause the fluctuation of acceleration time interval measurement, radar to constantly the rocket from the far point of the distance, because the noise radar makes the rocket range measurements with noise. Now, the real distance, velocity and acceleration of the rocket are obtained by measuring the distance of the rocket by radar.
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| Filename | Size | Date |
|---|
| 卡尔曼滤波法.txt | 2425 | 2017-11-20 |
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