Unmanned aerial vehicle testing equipment. According to GB 42590-2023 "Safety for Civil Unmanned Aerial Vehicle Systems";

GB/T38930-2020 "Wind Resistance Requirements and Test Methods for Civil Light Small Unmanned Aerial Vehicle Systems";

GB/T 38058-2019 "Test Methods for Civil Multi-rotor Unmannederial Vehicle Systems".

Civil UAV test standards.

Product description: The UAV free flight test bench is used for free flight testing of large UAVs. It can freely on the three axes of roll (Roll), pitch (Pitch), and yaw (Yaw), flexibly and efficiently carrying out UAV flight dynamics tests, ensuring the safety of the UAV itself. The test bench is compatible with a variety of multi-rotor types and size specifications of UAVs, with a rotor spacing of 40mm to 600mm, and supports a maximum rotation diameter of 1000mm.

Detailed introduction

The UAV free flight test bench is used free flight testing of large UAVs. It can freely rotate on the three axes of roll (Roll), pitch (Pitch), and yaw (Yaw) flexibly and efficiently carrying out UAV flight dynamics tests, while ensuring the safety of the UAV itself. The test bench is compatible with a variety of multi-rotor types and size of UAVs, with a rotor spacing of 450mm to 600mm, and supports a maximum rotation diameter of 1000mm. At same time, it supports the expansion of sensor suites to enhance the test performance of the test bench: the electronic sensor device suite high-resolution absolute magnetic encoder (multiple turns) will and save your test data in real-time and accurately. The system can be directly connected to a PC computer through MATLAB and Simulink to maximize the acceleration of the UAV and validation process. The intelligent motor suite test platform's intelligent motor can actively control the speed, angular position, and torque of the UAV body through current or voltage. The control can be adjusted and customized, supporting the control of the speed and response intensity of any single motor.

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