Intel Aero Ready to Fly UAV
KEY AIRCRAFT AND SYSTEMS NOTES
Specifications
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Voltage Input 11.1 - 14.8V
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Intel Aero Compute Board
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Intel® AtomTM x7-Z8750 processor, 4 GB
LPDDR3-1600, 32 GB eMMC
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Dual Band Wireless-AC 8260
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MicroSD slot
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M.2 connector 1 lane PCIe for SSD
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USB 3.0 OTG
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Programmable I/O via Altera Max 10 FPGA
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Insyde Software InsydeH2O UEFI BIOS
optimized for Aero Platform
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Dronecode PX4 autopilot (STM32 MCU, MAVLink
protocol over HSUART)
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Sensors
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Intel RealSense camera (R200)
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8MP RGB camera (front-facing)
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down-facing monochrome VGA camera w/
global shutter
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6 degrees of freedom (DoF) inertial
measurement unit (IMU)
Use Notes
Use credible brand lithium-Ion polymer (Li-Po) 4 cell 14.4v (4S) 4000mAh+ (with XT60 connector).
Charge with credible brand charger. Battery must be secured tightly in the cavity with velcro straps.
battery shifts, control may be lost.
Test UAV balance at frame side center points with battery inserted. Adjust forward or backward for
best balance.
O ut of balance airframes add pressure to autopilots unnecessarily using battery
capacity to compensate.
GPS array mast may be stiff. Grip mast at center to raise 90
spins to fully secure.
Attach Yuneec Typhoon H 230mm props noting A and B types:
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A-types
attach to motors with black caps by gripping motor and pressing down on the prop and twisting
counter-clockwise (per the arrows on the prop).
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B-types
a ttach to motors with white caps by gripping motor and pressing down on the prop and twisting
clockwise (per the arrows on the prop).
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Magnetometer
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Altitude
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GPS
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compass
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Props Yuneec Typhoon H 230mm
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Spektrum* DSMX* Serial Receiver
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Spektrum DXe Transmitter (2.4GHz DSMX
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Flight time: 20 min (4S 4000mAh battery,
hovering, no added payload)
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Max sustained wind: 15 knots
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Max control range: 300m
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Max airspeed: 15 m/s
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Max operational altitude: 5000msl
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Temperature range (min / max): -0 C / +45 C
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Weight without battery: 865g
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Max takeoff gross weight: 1900g
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Width: 360 mm (hub-to-hub)
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Height: 222 mm (base to top of GPS arra
°
. Tightening clamp may take several
I f
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