FIELD: aviation.
SUBSTANCE: multi-rotor type UAV systems complex testing and adjustment stand contains a base on which a ball hinge mounting part is located, into which a cylinder with a ball hinge is inserted, equipped with a self-levelling mechanism with rubber dampers, as well as a clamping limiting nut for fixing the cylinder, a piston with a platform, a lock nut of the piston, a strain gauge, a fastening plate and a processing and display module.
EFFECT: enabling the possibility to simulate all flight modes of the UAV, as well as to check the maximum weight of the payload, which it is capable of lifting.
4 cl, 4 dwg
