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# md4-1000 From microdrones Revision as of09:50, 23 June 2014 by Tobias Matschke (Talk 

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## I Newer revision ---+ ( diff:) The microdrones are AUMAV (Autonomous Unmanned Micro Aerial Vehicle) designed to perform tasks in the field of documentation, coordination, exploration, survey ing, communication, inspection and observa tion. They are miniaturised VTOL-aircraft (Vertical Take Off and Landing) based on the quadrocopter principle. Every microdrone can fly by radio 

### link command & control or autonomously with the aid of our GPS Waypoint navigation system Thanks to the unique AAHRS (Attitude, Altitude and Heading Reference System) even completely inexperienced pilots can learn to fly the microdrones in a very short time. Usually a beginner is able to control the microdron e after less than one hour of training. A modular payload concept allows us, to flexibly adapt the equipment to the intended mission. The availability of a high resolution digital sti ll camera, several video solutions adapted to very different li ghting conditions and also a high-end thermography heat imaging system s ensures the capability to carry out miscellaneous tasks of image recording and image broadcasting. The basic system consists of the microdrone with batteries, C&C and payloads in its transport box as well as the basestation suitcase. microdrones' second product i s the md4-l 000 which is on the market since late 2009. 

# Sound emission • 71 , 0 dBa @ 3m • 44,2 dBa @ 50m • 37 , 8 dBa @ lOOm 

# Current Payloads • SonyNEX-7 • Sony HDR-CX740VE • Olympus E-P3 • Panasonic HDC SD-909 • Day li ght Camera • Dawn (near IR) Camera • FLIR Tau 640 • TetraCam ADC Lite • TetraCam MiniMCA 6 • GfG Microtector II G460

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## Discontinued Payloads • Olympus E-P2 • Olympus E-Pl Retrieved from "http: // wiki.microdrones.com /index.php?title=md4-1 OOO&oldid= 815" Categories: Pr oduct microdrone http: / / wiki . microdrone s.com /index. php?title=md4 -l OOO&oldid = 815&p...

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# __ md4 - 1000 Article No. MD -02-001 

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Description: microdrones medium s ized quadrocopter Technical Specifications Vehicle mass: Payload mas s (recommended): Payload mass (maximum): Maximum take-off weight: Battery: C limb rate: Cruising speed: Peak thru st:
Endurance:
Flight radius: Service ceiling: 2650g 800g 1200g 6000g 6S2P LiPo , 22.2V , 13000mAh 7.5 m /s 1 2 .0 m/s 118.0N up to 88min with special high endurance configuration End urance can always vary with wind/weather , payload and age of battery with 800g payload the average is 45 minutes min. 500m on C&C 

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max. 20km on WP

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### - 2000 m ASL 4500m ASL - 3-blade carbon 

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Temperature range: Humidity: rotors necessary Operational Conditions ------i 

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# so o c max 90% r.H. Wind tolerance : stea dy picture s up to 6 m/s max. up to 12 m/ s

**~** Diameter: Height: Dimensions 1030mm 500mm

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