Program Flight Dynamics :

Solving the coupled non-linear six degrees of freedom ordinary differential equations of motion

Program Abilities :

• Calls program Airloads® to calculate aerodynamic , environment and powerplant forces and moments in the body fixed coordinate system

• Position and attitude of the flying vehicle

• Translational and rotational velocities in global and body coordinate systems

• Translational and rotational accelerations in global and body coordinate systems

• Transformation matrix from global to body coordinate system

• Matlab Simulink with Virtual Reality toolbox to integrate and animate all the calculations at each time step