Uav reliability test uav reliability test facility
When it comes to drones, most people probably think of aerial photography.In fact, with China's uav industry at the forefront of the world, the application of uav has been greatly expanded.As a "flying robot", drones can replace human aerial scene operation, greatly improving the efficiency and security of work.In recent years, unmanned aerial vehicles (uavs) have made great achievements in electric power equipment inspection, agricultural disaster prediction, land survey and other fields.Because no one unit operation environment conditions often changeable and complex, and each device for internal heating power consumption control, eventually lead to craft their own hardware for can adapt to different temperature, so in order to meet the demand of more homework or specific conditions, high and low temperature under the condition of flight test is a must.Here is a summary of some of the drone reliability tests given by united testing:
Uav high and low temperature test
Because no one unit operation environment conditions often changeable and complex, and each device for internal heating power consumption control, eventually lead to craft their own hardware for can adapt to different temperature, so in order to meet the demand of more homework or specific conditions, high and low temperature under the condition of flight test is a must.Can't say, aircraft flying in the south there is no problem, but to the north cannot take off, or unmanned aerial vehicle (uav) under the condition of high temperature or low temperature storage, aircraft was the unknown fault, and so on, for ordinary consumers, the result is not acceptable.United testing high and low temperatures
Drone drop test
Drop test is currently the vast majority of products all need to do a routine test, on the one hand is to test whether unmanned aerial vehicle (uav) packing of the products can well protect the product itself in order to ensure transportation safety;On the other hand is the hardware reliability of aircraft, aircraft, after all, as a commonly used smartphone, inevitably there will be a minor knock small touch, or even unexpected breaking machine, performance and reliable hardware can greatly enhance the aircraft for the resistance of the outside world, will be the machine damage to a minimum, reduce maintenance time and costs.
Drone vibration test
Drones inside there are a lot of sensors, such as the IMU inertial measurement unit, the data of perception if vibration affected because it is over, the end result is the aircraft may be "crazy", completely uncontrolled;Secondly, the internal hardware structure is complex, and the integration strength of the fuselage is high. If the vibration results in abnormal hardware connection, loose screws or modules, etc., it is not acceptable.At the same time, the vibration of the aircraft itself will affect the stability of flight and the effect of aerial photography.Want to know, if you often go out, the road will be affected by vehicle bumps vibration, take-off and landing is not smooth or often party will also be affected by the vibration, so the aircraft for vibration resistance should not be neglected.
Uav testing reference standards:
GJB 2347-1995 general specifications for uav
GJB 3060-1997 general specifications for unmanned aerial vehicle electrical systems
GJB 5433-2005 general requirements for uav systems
GJB 5434-2005 general requirements for uav system flight test
GJB 5435-2005 uav strength and rigidity specification
General requirements for GJB 6703-2009 uav measurement and control system
Uav high and low temperature test
Because no one unit operation environment conditions often changeable and complex, and each device for internal heating power consumption control, eventually lead to craft their own hardware for can adapt to different temperature, so in order to meet the demand of more homework or specific conditions, high and low temperature under the condition of flight test is a must.Can't say, aircraft flying in the south there is no problem, but to the north cannot take off, or unmanned aerial vehicle (uav) under the condition of high temperature or low temperature storage, aircraft was the unknown fault, and so on, for ordinary consumers, the result is not acceptable.United testing high and low temperatures
Drone drop test
Drop test is currently the vast majority of products all need to do a routine test, on the one hand is to test whether unmanned aerial vehicle (uav) packing of the products can well protect the product itself in order to ensure transportation safety;On the other hand is the hardware reliability of aircraft, aircraft, after all, as a commonly used smartphone, inevitably there will be a minor knock small touch, or even unexpected breaking machine, performance and reliable hardware can greatly enhance the aircraft for the resistance of the outside world, will be the machine damage to a minimum, reduce maintenance time and costs.
Drone vibration test
Drones inside there are a lot of sensors, such as the IMU inertial measurement unit, the data of perception if vibration affected because it is over, the end result is the aircraft may be "crazy", completely uncontrolled;Secondly, the internal hardware structure is complex, and the integration strength of the fuselage is high. If the vibration results in abnormal hardware connection, loose screws or modules, etc., it is not acceptable.At the same time, the vibration of the aircraft itself will affect the stability of flight and the effect of aerial photography.Want to know, if you often go out, the road will be affected by vehicle bumps vibration, take-off and landing is not smooth or often party will also be affected by the vibration, so the aircraft for vibration resistance should not be neglected.
Uav testing reference standards:
GJB 2347-1995 general specifications for uav
GJB 3060-1997 general specifications for unmanned aerial vehicle electrical systems
GJB 5433-2005 general requirements for uav systems
GJB 5434-2005 general requirements for uav system flight test
GJB 5435-2005 uav strength and rigidity specification
General requirements for GJB 6703-2009 uav measurement and control system
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