Using STM32H753IIK6 processor, double
precision floating point arithmetic unit
(DSP&FPU), the main frequency up to 480MHz;
2M FLASH,1MB RAM; For Autopilot
to bring powerful computing power, rapid
data processing ability, for more functional
development and flight stability to provide
more possibilities
With three redundant IMUs and two redundant barometers on separate
buses, when one set of IMUs fails, the system seamlessly switches to
another reliable IMU
High-speed communication with task
computers through Ethernet; In the future,
high-end links, INS and high-end mapping
cameras can be connected through
Ethernet to meet the needs of high-end
unmanned system
Main Specification | |
---|---|
Hardware Standard |
Pixhawk FMUv6x Standard DS-010 Pixhawk AutoPilot Bus Standard DS-012 Pixhawk AutoPilot V6X Standard |
Processor |
STM32H753IIK6 32-bit Arm® Cortex®-M7 480MHz MCUs, 2MB Flash,1MB RAM |
Coprocessor | STM32F10X |
Accelerometer&Gyroscope |
ICM42688-P ICM-20649 BMI088 |
Compass | RM3100 |
Barometer | 2×ICP-20100 |
Interfaces | |
PWM I/O | 16 |
Power | 4 2 for UAVCAN,2 for SMBUS (I2C) |
GPS | 2 1 GPS port with I2C and safety switch (GPS1) 1 interface with I2C and GPS (GPS2) |
TELEM | 3 |
CAN | 2 |
PPM RC | 1, Dedicated R/C input for PPM |
SBUS/DSM/RSSI | 1 Dedicated R/C input for Spektrum / DSM and S.Bus with analog / PWM RSSI input |
SBUS outs | 1 |
FMU Debug | 1 |
IO Debug | 1 |
Ethernet | 1 |
SPI EXTERNAL1 | 1 (SPI6 interface,for expanding external sensors) |
ADIO | 1 AD3.3/ADC6.6 |
UART4 | 1 |
USB | 2 1 for Type C 1 for GH interface USB |
TF Slot | 1 |
Physical characteristics | |
Operating voltage | 4.75~5.45V |
Servo input voltage | 0~9.9V |
Operating temperature | -20~85 |
Size | 45×90×29.2mm |
Weight | 99g Core:43g Baseboard:56g |
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