Battery Requirements |
LiPo, 3S or 4S, XT60 connector |
|
Max dimensions (mm): 150 x 50 x 32 |
Required accessories |
Micro HDMI to standard HDMI cable and HDMI monitor |
|
Support for USB 2.0 peripherals: |
|
Selfpowered USB 2.0 Hub |
|
OTG Cable1: USB 2.0 MicroB to TypeA female |
|
USB keyboard |
|
USB 2.0 flash drive 2GB or larger for firmware
updates |
Optional Accessories |
USB mouse |
|
Support for USB 3.0 peripherals: |
|
Selfpowered USB 3.0 Hub |
|
OTG cable2: (nonstandard) USB3.0 MicroB to TypeA
female |
|
1 This is the same cable supplied with the Intel Aero
Compute Board |
|
2 Available as an accessory through Intel (coming
soon) |
The Intel Aero Ready to Fly Drone includes the following |
Intel Aero Compute Board |
|
Intel Atom x7Z8750 processor |
|
4 GB LPDDR31600 |
|
32 GB eMMC |
|
MicroSD* memory card slot |
|
M.2 connector 1 lane PCIe for SSD |
|
Intel Dual Band WirelessAC 8260 |
|
USB 3.0 OTG |
|
Reprogrammable I/O via Altera Max 10 FPGA |
|
8MP RGB camera (frontfacing) one of the 3 camera modules included with the Aero Vision Accessory Kit |
|
VGA camera, global shutter, monochrome
(downfacing) |
|
Opensource embedded Linux*, Yocto Project |
|
Insyde Software InsydeH2O* UEFI BIOS optimized for the Intel Aero Platform for UAVs. More about InsydeH20* |
|
Intel RealSense camera (R200) |
|
Intel Aero Flight Controller with Dronecode* PX4*
autopilot |
|
STM32* microcontroller |
|
Temperature compensated: 6 DoF IMU, magnetometer, and altitude
sensors |
|
Connected to the Aero Compute board over HSUART and communicates using MAVLink* protocol |
|
Preassembled quadcopter |
|
Carbon fiber airframe |
|
GPS and compass |
|
Power distribution board |
|
4 electronic speed controllers |
|
4 motors |
|
8 snapon propellers |
|
Spektrum* DSMX* Serial Receiver |
|
Spektrum DXe Transmitter (2.4GHz DSMX) |
Other Specifications |
The Intel Aero Ready to Fly Drone is a platform for developers and is intended to be modified by developers according to their professional judgment. Intel has not established operating limitations for this drone development platform, or tested any configurations other than the base configuration as shipped. Developers are responsible for testing and ensuring the safety of their own configurations, and establishing the operating limits of those configurations. |
Dimensions: hubtohub |
360 mm |
Drone Height base to top of GPS antenna |
222 mm |
Propeller (Yuneec Typhoon H) Length |
230 mm |
Weight of Drone basic configuration without battery |
865 g |
Gross Weight (max) max takeoff
weight |
1900 g |
Flight Time (max) with 4S, 4000mAh battery, hovering, no added payload |
20 min |
Maximum Sustained Wind |
15 knots |
Maximum Control Distance with supplied remote
control |
300 m |
Airspeed (max) |
15 m/s |
Altitude of Operation (max) height above sea level |
4500 m |
Flight Height Limit (max) height Above Ground Level (AGL) |
122 m |
Outside Air Temperature (min /
max) |
0 C / +45 C |
ESC and Motor designed and manufactured by Yuneec, modified for |
|
Intel Aero |
|
Input control interface |
UART |
Input voltage range |
11.1 14.8V |