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 |
Topics
- Fundamental Coordinate System Concepts
Define coordinate systems when working with the Aerospace Blockset™ software.
