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6DOF

Implement six-degrees-of-freedom equations of motion in simulations, using Euler angles and quaternion representations

Model and simulate point mass and six-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

6DOF (Euler Angles)Implement Euler angle representation of six-degrees-of-freedom equations of motion
6DOF (Quaternion)Implement quaternion representation of six-degrees-of-freedom equations of motion with respect to body axes
6DOF ECEF (Quaternion)Implement quaternion representation of six-degrees-of-freedom equations of motion in Earth-centered Earth-fixed (ECEF) coordinates
6DOF Wind (Quaternion)Implement quaternion representation of six-degrees-of-freedom equations of motion with respect to wind axes
6DOF Wind (Wind Angles)Implement wind angle representation of six-degrees-of-freedom equations of motion
Custom Variable Mass 6DOF (Euler Angles)Implement Euler angle representation of six-degrees-of-freedom equations of motion of custom variable mass
Custom Variable Mass 6DOF (Quaternion)Implement quaternion representation of six-degrees-of-freedom equations of motion of custom variable mass with respect to body axes
Custom Variable Mass 6DOF ECEF (Quaternion)Implement quaternion representation of six-degrees-of-freedom equations of motion of custom variable mass in Earth-centered Earth-fixed (ECEF) coordinates
Custom Variable Mass 6DOF Wind (Quaternion)Implement quaternion representation of six-degrees-of-freedom equations of motion of custom variable mass with respect to wind axes
Custom Variable Mass 6DOF Wind (Wind Angles)Implement wind angle representation of six-degrees-of-freedom equations of motion of custom variable mass
Simple Variable Mass 6DOF (Euler Angles)Implement Euler angle representation of six-degrees-of-freedom equations of motion of simple variable mass
Simple Variable Mass 6DOF (Quaternion)Implement quaternion representation of six-degrees-of-freedom equations of motion of simple variable mass with respect to body axes
Simple Variable Mass 6DOF ECEF (Quaternion)Implement quaternion representation of six-degrees-of-freedom equations of motion of simple variable mass in Earth-centered Earth-fixed (ECEF) coordinates
Simple Variable Mass 6DOF Wind (Quaternion)Implement quaternion representation of six-degrees-of-freedom equations of motion of simple variable mass with respect to wind axes
Simple Variable Mass 6DOF Wind (Wind Angles)Implement wind angle representation of six-degrees-of-freedom equations of motion of simple variable mass

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