- Category:
- matlab
- Tags:
-
[Matlab]
[源码]
- File Size:
- 2kb
- Update:
- 2016-06-27
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- Uploaded by:
- 朱曙光
Description: This based on the Czech Republic and even the four elements Inertial Navigation System program algorithm method, a method of angular increments > aircraft during flight fly height unchanged > heading counterclockwise positive > in the Geography Department of the navigation frame > Run than the force required to import information and recommendations gyro angular rate information program
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04699422SimulationSINS
......................\SINS.m
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