- Category:
- matlab
- Tags:
-
[Matlab]
[源码]
- File Size:
- 5kb
- Update:
- 2016-05-08
- Downloads:
- 0 Times
- Uploaded by:
- 桂小
Description: Numerical solution of differential equations method, It draws on principal component analysis algorithm (PCA), It comprises aircraft flight attitude control, such as slip angle, tilt angle, roll angle, pitch angle.
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