Modular Aircraft Design and Flight Simulation (MADAFS)
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