Spacecraft Rigid Body Dynamics (attitude) library block
by Paul Acquatella
21 Apr 2011
(Updated 22 Apr 2011)
This library block for simulation (academic purpose) computes the attitude dynamics of a rigid body
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| File Information |
| Description |
The dynamics of the rotational motion of a rigid body is simulated with this functional library block. This block is intended for simulation (academic) purposes, where the time history of the angular velocity vector is provided.
This library block is part of a library currently being developed for the simulation of spacecraft attitude control systems. |
| Required Products |
Simulink
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| MATLAB release |
MATLAB 7.11 (2010b)
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| Updates |
| 21 Apr 2011 |
corrected a typo in the description |
| 21 Apr 2011 |
corrected typo on the description |
| 22 Apr 2011 |
updated screenshot |
| 22 Apr 2011 |
update |
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