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Peter Barker b751224ae1 hwdef: don't include solo gimbal or oreoled on thepeach autopilots 2023-08-29 11:14:15 +10:00
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README.md
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hwdef-bl.dat hwdef: remove uart7 from thepeach-k1 bootloader to get it compiling 2023-04-22 13:58:02 +10:00
hwdef.dat hwdef: don't include solo gimbal or oreoled on thepeach autopilots 2023-08-29 11:14:15 +10:00
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README.md

ThePeach FCC-K1

:::warning Ardupilot does not manufacture this (or any) autopilot. Contact the manufacturer for hardware support or compliance issues. :::

ThePeach FCC-K1 is an advanced autopilot designed and manufactured in ThePeach.

ThePeach FCC-K1

Specifications

  • Main Processor: STM32F427VIT6

    • 32bit ARM Cortex-M4, 168 MHz 256 KB RAM 2 MB Flash memory

  • IO Processor: STM32F100C8T6

    • ARM Cortex-M3, 32bit ARM Cortex-M3, 24 MHz, 8KB SRAM

  • On-board sensors

    • Accel/Gyro: ICM-20602
    • Accel/Gyro/Mag: MPU-9250
    • Barometer: MS5611

  • Interfaces

    • 8+5 PWM output (8 from IO, 5 from FMU)
    • Spektrum DSM / DSM2 / DSM-X Satellite compatible input
    • Futaba S.BUS compatible input and output
    • PPM sum signal input
    • Analogue / PWM RSSI input
    • S.Bus servo output
    • Safety switch/LED
    • 4x UART Ports: TELEM1, TELEM2, GPS, SERIAL4
    • 2x I2C Ports
    • 1x CAN bus
    • 1x ADC
    • Analog inputs for voltage / Current of 1 battery

  • Mechanical

    • Dimensions: 40.2 x 61.1 x 24.8 mm
    • Weight: 65g

Connectors

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Serial Port Mapping

UART Device Port
USART1 /dev/ttyS0 IO Processor Debug
USART2 /dev/ttyS1 TELEM1 (flow control)
USART3 /dev/ttyS2 TELEM2 (flow control)
UART4 /dev/ttyS3 GPS1
USART6 /dev/ttyS4 PX4IO
UART7 /dev/ttyS5 Debug Console
UART8 /dev/ttyS6 TELEM4

Voltage Ratings

ThePeach FCC-K1 can be double-redundant on the power supply if two power sources are supplied. The two power rails are: POWER and USB.

:::note The output power rails FMU PWM OUT and I/O PWM OUT do not power the flight controller board (and are not powered by it). You must supply power to one of POWER or USB or the board will be unpowered. :::

Normal Operation Maximum Ratings

Under these conditions all power sources will be used in this order to power the system:

  1. POWER input (5V to 5.5V)
  2. USB input (4.75V to 5.25V)

Absolute Maximum Ratings

Under these conditions, all power sources cause permanent damage to the flight controller.

  1. POWER input (5.5V Over)
  2. USB input (5.5V Over)

Where to buy

Order from ThePeach