Medium and low altitude flying unmanned aerial vehicle monitoring system

The invention discloses a medium and low altitude flying unmanned aerial vehicle monitoring system. The medium and low altitude flying unmanned aerial vehicle monitoring system comprises a ground power supply assembly and an aircraft, wherein the ground power supply assembly comprises a ground elect...

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Bibliographische Detailangaben
Hauptverfasser:	ZHANG TAO, ZHAO DONGKAI, LI GUOSHENG, HAN JINJIE, GUO WENLIN
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AEROPLANES AIRCRAFT ANALOGOUS ARRANGEMENTS USING OTHER WAVES ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COLORIMETRY COSMONAUTICS DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES ELECTRIC COMMUNICATION TECHNIQUE ELECTRIC EQUIPMENT OR PROPULSION OF ELECTRICALLY-PROPELLEDVEHICLES ELECTRICITY ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES, IN GENERAL EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION ORRERADIATION OF RADIO WAVES MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES MEASUREMENT OF INTENSITY, VELOCITY, SPECTRAL CONTENT,POLARISATION, PHASE OR PULSE CHARACTERISTICS OF INFRA-RED,VISIBLE OR ULTRA-VIOLET LIGHT MEASURING PARACHUTES PERFORMING OPERATIONS PHYSICS PICTORIAL COMMUNICATION, e.g. TELEVISION RADIATION PYROMETRY RADIO DIRECTION-FINDING RADIO NAVIGATION TESTING TRANSPORTING VEHICLES IN GENERAL
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Beschreibung
Zusammenfassung:	The invention discloses a medium and low altitude flying unmanned aerial vehicle monitoring system. The medium and low altitude flying unmanned aerial vehicle monitoring system comprises a ground power supply assembly and an aircraft, wherein the ground power supply assembly comprises a ground electricity supply module, a low-voltage electricity supply module and a high-voltage line, a mooring cable internally comprises an electricity supply wire and two single mode fibers, a support is arranged on one side of the ground power supply assembly, a wire winding box is arranged on the support, a thermal imager, a visible light high-definition camera and a laser range finder are arranged in a monitoring box, and a central processing unit module, a GPS positioning module, a Beidou positioning module, a data transmission module and an alarm chip which are connected with one another are arranged in a control box correspondingly. According to the medium and low altitude flying unmanned aerial vehicle monitoring system