The following features are available using this framework: 

• V-h diagram

• Aircraft performance analysis in the full flight envelope

• Aircraft sizing from the first principle

• Aerodynamic derivative estimation and stability analysis, dynamic mode analysis, 

• Frequency domain analysis of the aircraft (open-loop)

•  Control surface sizing based on aircraft rate requirements 

• Aircraft six-degree-of-freedom simulation for time history examination

• Impact of wind, gust, and turbulence effect on aircraft natural response

• V-n diagram

• Aircraft wing load analysis (Shear force and Bending Moment) 

•  Handling quality check

• Identifies the critical flight parameters that need to be addressed to minimize the possible occurrence of accidents of unmanned aircraft