6DOF

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

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

Topics

About Aerospace Coordinate Systems

Define coordinate systems to represent aircraft and spacecraft motion.

Featured Examples

Six Degree of Freedom Motion Platform

How to connect an Aerospace Blockset™ six degree of freedom equation of motion block.

Open Model

Aerospace Blockset Documentation

Support

Try MATLAB, Simulink, and Other Products

Get trial now