- Category:
- matlab
- Tags:
-
[Matlab]
[源码]
- File Size:
- 11kb
- Update:
- 2016-01-23
- Downloads:
- 0 Times
- Uploaded by:
- 王达从
Description: Based on three-axis attitude control of the spacecraft, according to the actual situation, fully taking into account the dynamic and kinematic coupling triaxial, can be controlled separately for each angular pose
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dynamic_control\control.m
...............\kinematics.m
...............\yuhndongxue.mdl
dynamic_control
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