Design Specification 5
✍️Bench: Aircraft Tests
Propose a layout solution for the design of a mechanism to measure aerodynamic loads and the aircraft damping system.
UAV - Vtol type, with a take-off weight up to 30 kg, mounted on the roof of a car moving in the speed range of 70-120 km/h. Purpose: The aircraft must strive to maintain its position while the vehicle is moving, by means of aerodynamic surfaces use and the aircraft power plant.
Define parameters as follows:
Required free movements of the aircraft along its axes;
Applicable sensors and measuring devices.
Wing/drag ratio.
Create a sensor connection diagram.
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