6DOF

R2026b

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