sUAS Performance Prediction Software

Prediction results accurate to within < 5%

Allows for rapid, educated decision making in mission critical scenarios

Quickly determine the ideal cruise speed for maximized range and flight time

Takes into account a multitude of CFD, battery, and power system factors

Outputs concise and easy-to-understand data for flight performance as well as stats that can be directly used for TECS tuning and trim parameters in Ardupilot/PX4

Rapid assessment of configuration changes such as added payload weight, power consumption, or battery

Accurate prediction of battery mass as well as AUW (all-up-weight)

Optimized for all fixed-wing sUAS from 3D-Printed to composite with varying skin friction

Simulation run-time < 20ms per run

Fully functional in internet denied environments

Runs on MacOS, Windows and Linux

Ability to export results directly to CSV

Ability to view multiple aircraft configurations side by side with tabbed UI

Ability to save and load aircraft configuration files as well as view multiple side by side

Includes software updates as well as customer support throughout the license period

Determine difference in range between different battery and payload options

Determine difference in endurance between different battery and payload options

Minimize ArduPilot/PX4 setup time with known trim pitch, trim airspeed and TECS parameters

Determine if an airframe will be hand-launchable and belly-landable based on stall speed and wingloading

Determine increase/decrease in climb rate based on increase/decrease in weight and/or power

Optimize new aircraft designs for minimized drag and maximized range/endurance

Easily provide customers/stakeholders with a variety of flight performance stats based on varying configurations of the airframe

Compare differences in performance at high altitude vs low altitude or different air densities