CN-121990176-A - Unmanned aerial vehicle testing device and control method

CN121990176ACN 121990176 ACN121990176 ACN 121990176ACN-121990176-A

Abstract

The invention discloses an unmanned aerial vehicle testing device and a control method, and relates to the technical field of unmanned aerial vehicle testing, wherein the unmanned aerial vehicle testing device comprises a base, a steering part and a flexible connecting part; the steering piece is arranged on the upper side of the base, the steering piece is used for installing the unmanned aerial vehicle and enabling the unmanned aerial vehicle to move relative to the base, and two ends of the flexible connecting piece are connected with the steering piece and the base. The unmanned aerial vehicle steering device is provided with the base for fixing the unmanned aerial vehicle, the steering piece is arranged on the base, the unmanned aerial vehicle can be mounted on the base, and the unmanned aerial vehicle can move relative to the base through the steering piece, meanwhile, the unmanned aerial vehicle steering device is also provided with the flexible connecting piece, two ends of the flexible connecting piece are respectively connected with the steering piece and the base, and when the steering piece and the unmanned aerial vehicle are out of control, fast spinning or breaking and releasing are caused, the flexible connecting piece can pull and limit the movement of the unmanned aerial vehicle and the steering piece, and property loss and personal injury caused by the out of control of the steering piece and the unmanned aerial vehicle are avoided.

Inventors

WANG BINGXIN
GENG DONGLIANG
LIN JIN

Assignees

菲亚兰德智能(深圳)有限公司

Dates

Publication Date: 20260508
Application Date: 20260306

Claims (10)

1. An unmanned aerial vehicle testing arrangement, characterized in that includes: A base; a steering member mounted on the upper side of the base for mounting the unmanned aerial vehicle and enabling the unmanned aerial vehicle to move relative to the base, and And two ends of the flexible connecting piece are connected with the steering piece and the base.
2. The unmanned aerial vehicle testing device of claim 1, wherein the steering member comprises: A universal joint mounted to the base, and The mounting seat is connected with the universal joint and used for mounting the unmanned aerial vehicle, and can move relative to the base through the universal joint, and two ends of the flexible connecting piece are connected with the mounting seat and the base.
3. The unmanned aerial vehicle testing apparatus of claim 2, wherein the gimbal comprises: the middle part of the limiting plate is provided with clamping holes, two limiting plates are arranged at intervals and are connected with each other through connecting rods, and The universal ball is clamped between the two limiting plates and is provided with a connecting part, the connecting part penetrates through the clamping hole of one of the limiting plates and is connected with one of the base and the mounting seat, and the other of the base and the mounting seat is connected with the other of the two limiting plates.
4. The unmanned aerial vehicle testing device of claim 3, wherein the universal joint comprises pins, wherein a first jack matched with the pins is formed in the limiting plate of one of the pins, a second jack matched with the pins is formed in one of the base and the mounting seat, and the pins can penetrate through the second jack and the first jack to be plugged in and used for limiting the universal joint and the mounting seat.
5. The unmanned aerial vehicle testing device of claim 2, wherein the mount comprises: a connecting table connected with the universal joint, two ends of the flexible connecting piece are connected with the connecting table and the base, and The installing support, the installing support install in the connection platform, the installing support passes through screw hole and unmanned aerial vehicle bolted connection.
6. The unmanned aerial vehicle test apparatus of claim 5, wherein a plurality of the threaded holes are provided in the mounting bracket and are at least partially spaced vertically, the threaded holes at different heights being capable of forming different mounting combinations, and/or, The installing support is including the linking arm demountable installation is embraced the ring on the linking arm for supply unmanned aerial vehicle's girder spacing wearing to establish, the linking arm passes through screw hole and unmanned aerial vehicle bolted connection.
7. The unmanned aerial vehicle testing device of claim 6, wherein a plurality of the connecting arms are provided, and a temporary support plate is installed between a plurality of the connecting arms for supporting the unmanned aerial vehicle in an auxiliary manner.
8. The unmanned aerial vehicle testing device of claim 1, wherein the base comprises: a counterweight table for placing counterweight blocks, and The support frame is installed in the counter weight platform, the support frame with turn to the piece and be connected, the flexible connection piece connect in turn to the piece with the support frame.
9. A method of controlling a test of a drone, based on a drone test apparatus according to any one of claims 1 to 8, the method comprising the steps of: After the unmanned aerial vehicle is installed on the steering part of the unmanned aerial vehicle testing device, a test starting instruction is obtained to control the starting of the unmanned aerial vehicle; after the unmanned aerial vehicle is started, controlling the unmanned aerial vehicle to perform a single test, in the single test, controlling the unmanned aerial vehicle to enter a plurality of flight modes successively according to a preset time sequence relationship, and executing corresponding preset time length in each flight mode; after the single test is completed, controlling the unmanned aerial vehicle to repeatedly execute the single test until the total duration meets the preset test duration; and acquiring the operation parameters of the unmanned aerial vehicle in the test process, and performing aging evaluation by combining the mechanical loosening condition with a tester.
10. The method of claim 9, wherein the plurality of flight modes includes adjusting a flight attitude of the unmanned aerial vehicle to a first flight attitude and a second flight attitude, wherein the first flight attitude is a hover attitude of the unmanned aerial vehicle in which the plurality of wings are at a same horizontal plane and the second flight attitude is a flight attitude of the unmanned aerial vehicle that is tilted with respect to the horizontal plane, The operating parameters include at least one of an unmanned aerial vehicle control parameter, an unmanned aerial vehicle flight attitude parameter, an unmanned aerial vehicle temperature parameter, an ambient temperature parameter, and an ambient humidity parameter.

Description

Unmanned aerial vehicle testing device and control method Technical Field The invention relates to the technical field of unmanned aerial vehicle testing, in particular to an unmanned aerial vehicle testing device and a control method. Background In the current unmanned aerial vehicle production process, the stability, durability and consistency of products are controlled by enterprises respectively, and powerful test data support is lacked. Products need to be rapidly put on the market and are easily subjected to insufficient testing and batch difference fluctuation of incoming materials, so that quality fluctuation of final products occurs. Common testers are subjected to endurance test by the unmanned aerial vehicle in the external field through repeated test flight, and are subject to long charging time, noise disturbance of the generator, long period of the air-space declaration, high-temperature exposure to severe weather in windy and rainy days, high labor intensity and low efficiency, and the testers usually lack effective safety protection. Some enterprises adopt the crane overhead test to verify the stability of the front stage of flight control, avoid the large loss caused by the frying machine, delay the test progress, change the battery with effort, afford heavy vehicles are troublesome, and open outdoor sites are needed, the wind and rain are blown down in bad weather, the test cost is high, and the working efficiency is low. There are also few enterprises that have adopted indoor bench test, however such indoor bench structure often needs to cooperate unmanned aerial vehicle to carry out the durable test of high strength, easily leads to unmanned aerial vehicle to damage or lead to unmanned aerial vehicle out of control because of the device fracture, has the potential safety hazard. Disclosure of Invention The invention mainly aims to provide an unmanned aerial vehicle testing device and a control method, which aim to reduce the risk of out of control in unmanned aerial vehicle testing and improve the safety and stability in unmanned aerial vehicle testing. The unmanned aerial vehicle testing device comprises a base, a steering piece and a flexible connecting piece, wherein the steering piece is arranged on the upper side of the base and is used for installing an unmanned aerial vehicle and enabling the unmanned aerial vehicle to move relative to the base, and two ends of the flexible connecting piece are connected with the steering piece and the base. In one embodiment, the steering member comprises a universal joint and a mounting seat, wherein the universal joint is mounted on the base, the mounting seat is connected with the universal joint and used for mounting the unmanned aerial vehicle and can move relative to the base through the universal joint, and two ends of the flexible connecting member are connected with the mounting seat and the base. In one embodiment, the universal joint comprises a limiting plate and a universal ball, wherein clamping holes are formed in the middle of the limiting plate, two limiting plates are arranged at intervals and are connected with each other through a connecting rod, the universal ball is clamped between the two limiting plates, the universal ball is provided with a connecting part, the connecting part penetrates through the clamping hole of one of the limiting plates and is connected with one of a base and an installation seat, and the other of the base and the installation seat is connected with the other of the two limiting plates. In an embodiment, the universal joint comprises a plug, a first jack matched with the plug is formed in the limiting plate of one of the plugs, a second jack matched with the plug is formed in one of the base and the mounting seat, and the plug can penetrate through the second jack and be connected with the first jack in an inserting mode for limiting the universal joint and the mounting seat. In one embodiment, the mounting base comprises a connecting table and a mounting bracket, wherein the connecting table is connected with the universal joint, two ends of the flexible connecting piece are connected with the connecting table and the base, the mounting bracket is mounted on the connecting table, and the mounting bracket is connected with the unmanned aerial vehicle through a threaded hole in a bolt mode. In one embodiment, a plurality of threaded holes are formed in the mounting bracket, at least part of the threaded holes are arranged at intervals in the up-down direction, and threaded holes at different heights can form different mounting combinations. In an embodiment, be equipped with the linking arm on the installing support, demountable installation has the armful ring on the linking arm for supply unmanned aerial vehicle's girder spacing wears to establish, the linking arm passes through screw hole and unmanned aerial vehicle bolted connection. In an embodiment, the connecting arms are provided with a plura