3DOF

实现三个自由度方程tions 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)	实现三个自由度方程tions of motion with respect to body axes
3DOF (Wind Axes)	实现三个自由度方程tions of motion with respect to wind axes
Custom Variable Mass 3DOF (Body Axes)	实现三个自由度方程tions of motion of custom variable mass with respect to body axes
Custom Variable Mass 3DOF (Wind Axes)	实现三个自由度方程tions of motion of custom variable mass with respect to wind axes
Simple Variable Mass 3DOF (Body Axes)	实现三个自由度方程tions of motion of simple variable mass with respect to body axes
Simple Variable Mass 3DOF (Wind Axes)	实现三个自由度方程tions of motion of simple variable mass with respect to wind axes

Topics

About Aerospace Coordinate Systems
Define coordinate systems to represent aircraft and spacecraft motion.