Spacecraft Rigid Body Dynamics (attitude) library block

Version 1.6.0.0 (9.81 KB) by Paul Acquatella
This library block for simulation (academic purpose) computes the attitude dynamics of a rigid body
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969 Downloads
Updated 22 Apr 2011

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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.

Cite As

Paul Acquatella (2024). Spacecraft Rigid Body Dynamics (attitude) library block (https://www.mathworks.com/matlabcentral/fileexchange/31138-spacecraft-rigid-body-dynamics-attitude-library-block), MATLAB Central File Exchange. Retrieved .

MATLAB Release Compatibility
Created with R2010b
Compatible with any release
Platform Compatibility
Windows macOS Linux
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Version Published Release Notes
1.6.0.0

update
1.5.0.0

updated screenshot
1.2.0.0

corrected typo on the description
1.1.0.0

corrected a typo in the description
1.0.0.0