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3DOF

Implement three-degrees-of-freedom equations of motion in simulations, including custom variable mass models

Model and simulate point mass and three-degrees-of-freedom dynamics of fixed or variable mass atmospheric flight vehicles. Define representations of the equations of motion in body, wind, and Earth-centered, Earth-fixed (ECEF) coordinate systems. Transform between coordinate systems and perform unit conversions to ensure model consistency.

Blocks

3DOF (Body Axes)Implement three-degrees-of-freedom equations of motion with respect to body axes
3DOF (Wind Axes)Implement three-degrees-of-freedom equations of motion with respect to wind axes
Custom Variable Mass 3DOF (Body Axes)Implement three-degrees-of-freedom equations of motion of custom variable mass with respect to body axes
Custom Variable Mass 3DOF (Wind Axes)Implement three-degrees-of-freedom equations of motion of custom variable mass with respect to wind axes
Simple Variable Mass 3DOF (Body Axes)Implement three-degrees-of-freedom equations of motion of simple variable mass with respect to body axes
Simple Variable Mass 3DOF (Wind Axes)Implement three-degrees-of-freedom equations of motion of simple variable mass with respect to wind axes

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