GROUND UNMANNED AERIAL VEHICLE POWER SUPPLY NETWORK TESTING SYSTEM AND TESTING METHOD

The present invention relates to a ground unmanned aerial vehicle power supply network testing system and a testing method. A measurement and control channel of an engine is connected to an upper computer to transmit measurement and control data to the upper computer; an output end of the engine is...

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Hauptverfasser:	GUO, Yunceng, NIU, Zhenzhong, HUANG, Xiaodong, SUN, Xiaomiao
Format:	Patent
Sprache:	chi ; eng ; fre
Schlagworte:	ADVERTISING AIRCRAFT APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND,DEAF OR MUTE AVIATION COSMONAUTICS CRYPTOGRAPHY DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR DIAGRAMS DISPLAY EDUCATION EDUCATIONAL OR DEMONSTRATION APPLIANCES GLOBES GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR MEASURING MEASURING ELECTRIC VARIABLES MEASURING MAGNETIC VARIABLES PERFORMING OPERATIONS PHYSICS PLANETARIA SEALS TESTING TRANSPORTING
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creator	GUO, Yunceng NIU, Zhenzhong HUANG, Xiaodong SUN, Xiaomiao
description	The present invention relates to a ground unmanned aerial vehicle power supply network testing system and a testing method. A measurement and control channel of an engine is connected to an upper computer to transmit measurement and control data to the upper computer; an output end of the engine is connected in parallel to power supply input ends of a plurality of devices and power supply input ends of a plurality of electronic load simulators; and a fan speed sensor, a temperature acquisition module, and a current and voltage acquisition module are connected to the upper computer to transmit sensing signals to the upper computer. Engine speed drop parameters of a power supply network are tested when a high-power load is started, so as to evaluate the safety of the flight process and provide a reference for the optimization of a subsequent flight strategy. A heat source is effectively evaluated, and cable routing and heat dissipation design are guided and optimized. Whether each device works in the input volt
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language	chi ; eng ; fre
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subjects	ADVERTISING AIRCRAFT APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND,DEAF OR MUTE AVIATION COSMONAUTICS CRYPTOGRAPHY DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR DIAGRAMS DISPLAY EDUCATION EDUCATIONAL OR DEMONSTRATION APPLIANCES GLOBES GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR MEASURING MEASURING ELECTRIC VARIABLES MEASURING MAGNETIC VARIABLES PERFORMING OPERATIONS PHYSICS PLANETARIA SEALS TESTING TRANSPORTING
title	GROUND UNMANNED AERIAL VEHICLE POWER SUPPLY NETWORK TESTING SYSTEM AND TESTING METHOD
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