mirror of https://github.com/ArduPilot/ardupilot
257 lines
6.8 KiB
Markdown
257 lines
6.8 KiB
Markdown
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# Onboard FMU on Airvolute DCS2.Pilot board
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DroneCore 2.0 is a modular AI-driven open architecture autopilot designed for complex use cases that combines high computational processing power, redundant connectivity, small size, and low weight.The autopilot represents a one-stop-solution for developers integrating the functionality of carrier board, companion computer, and power distribution board into a single compact form factor.
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This system usually uses a "CUBE" autopilot as its primary FMU, but can use an onboard STM32H743 as the FMU. This board definition and firmware on `the ArduPilot firmware server <https://firmware.ardupilot.org>`__ is for this secondary FMU
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For more informations on DCS2.Pilot board see:
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https://docs.airvolute.com/dronecore-autopilot/dcs2
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## Where To Buy
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info@airvolute.com
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## Features
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- MCU: STM32H743
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- IMU: BMI088
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- Barometer: BMP390
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- 2 UARTS
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- 2 CAN buses
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- 4 PWM outputs
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- PPM (RC input)
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- external SPI and I2C
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- SD card connector
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- USB connection onboard with Jetson Host
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- Ethernet
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## DCS2.Pilot peripherals diagram
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<img width="957" alt="DC2 Pilot peripherals" src="https://github.com/vrsanskytom/ardupilot/blob/hwdef_for_airvolute_dcs2/libraries/AP_HAL_ChibiOS/hwdef/Airvolute-DCS2/DC2.Pilot%20peripherals.png">
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## DCS2.Pilot onboard FMU related connectors pinout
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### Top side
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<img width="818" alt="DCS2 Pilot_bottom" src="https://github.com/vrsanskytom/ardupilot/blob/hwdef_for_airvolute_dcs2/libraries/AP_HAL_ChibiOS/hwdef/Airvolute-DCS2/DCS2.Pilot_TopSide.png">
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#### <ins>PPM connector (RC input)</ins>
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JST GH 1.25mm pitch, 3-Pin
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Matching connector JST GHR-03V-S.
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RC input is configured on the PPM_SBUS_PROT pin as part of the PPM connector. Pin is connected to UART3_RX and also to analog input on TIM3_CH1. This pin supports all unidirectional RC protocols, but for it to be enabled, it is necessary to set SERIAL3_PROTOCOL as RCIN. Also RC input is shared with primary FMU, so it is default disabled on this secondary FMU.
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5V supply is limited to 1A by internal current limiter.
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<table border="1" class="docutils">
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<tbody>
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<tr>
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<th>Pin </th>
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<th>Signal </th>
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</tr>
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<tr>
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<td>1</td>
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<td>GND</td>
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</tr>
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<td>2</td>
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<td>5V</td>
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</tr>
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<td>3</td>
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<td>PPM</td>
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</tr>
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</tbody>
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</table>
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### Bottom side
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<img width="811" alt="DCS2 Pilot_top" src="https://github.com/vrsanskytom/ardupilot/blob/hwdef_for_airvolute_dcs2/libraries/AP_HAL_ChibiOS/hwdef/Airvolute-DCS2/DCS2.Pilot_BottomSide.png">
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#### <ins>FMU SEC. connector</ins>
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JST GH 1.25mm pitch, 12-Pin
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Matching connector JST GHR-12V-S.
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The DCS2 Onboard FMU supports up to 4 PWM outputs. These are directly attached to the STM32H743 and support all PWM protocols as well as DShot and bi-directional DShot.
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The 4 PWM outputs are in 2 groups:
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PWM 1,2 in group1
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PWM 3,4 in group2
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Channels within the same group need to use the same output rate. If any channel in a group uses DShot then all channels in the group need to use DShot.
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5V supply is limited to 1A by internal current limiter.
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<table border="1" class="docutils">
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<tbody>
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<tr>
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<th>Pin </th>
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<th>Signal </th>
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</tr>
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<tr>
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<td>1</td>
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<td>GND</td>
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</tr>
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<td>2</td>
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<td>GND</td>
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</tr>
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<td>3</td>
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<td>GPIO/PWM output 4</td>
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</tr>
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</tr>
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<td>4</td>
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<td>GPIO/PWM output 3</td>
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</tr>
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</tr>
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<td>5</td>
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<td>GPIO/PWM output 2</td>
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</tr>
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</tr>
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<td>6</td>
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<td>GPIO/PWM output 1</td>
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</tr>
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</tr>
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<td>7</td>
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<td>Serial 1 RX</td>
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</tr>
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</tr>
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<td>8</td>
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<td>Serial 1 TX</td>
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</tr>
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</tr>
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<td>9</td>
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<td>Serial 2 RX</td>
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</tr>
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</tr>
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<td>10</td>
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<td>Serial 2 TX</td>
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</tr>
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</tr>
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<td>11</td>
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<td>5V</td>
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</tr>
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</tr>
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<td>12</td>
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<td>5V</td>
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</tr>
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</tbody>
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</table>
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#### <ins>EXT. SENS. connector</ins>
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BM23PF0.8-10DS-0.35V connector
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Matching connector BM23PF0.8-10DP-0.35V
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This connector allows connecting external IMU with I2C and SPI data buses.
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5V supply is limited to 1.9A by internal current limiter.
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<table border="1" class="docutils">
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<tbody>
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<tr>
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<th>Pin </th>
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<th>Signal </th>
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</tr>
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<tr>
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<td>1</td>
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<td>SPI_MOSI</td>
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</tr>
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<td>2</td>
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<td>SPI_MISO</td>
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</tr>
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<td>3</td>
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<td>SPI_SCK</td>
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</tr>
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</tr>
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<td>4</td>
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<td>SPI_CS0</td>
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</tr>
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</tr>
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<td>5</td>
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<td>SPI_CS1</td>
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</tr>
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</tr>
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<td>6</td>
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<td>SPI_CS2</td>
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</tr>
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</tr>
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<td>7</td>
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<td>SPI_CS3</td>
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</tr>
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</tr>
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<td>8</td>
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<td>IMU_DRDY_EXT</td>
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</tr>
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</tr>
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<td>9</td>
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<td>I2C_SE_SDA</td>
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</tr>
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</tr>
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<td>10</td>
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<td>I2C_SE_SCL</td>
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</tr>
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</tr>
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<td>MP1</td>
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<td>5V</td>
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</tr>
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</tr>
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<td>MP2</td>
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<td>5V</td>
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</tr>
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</tr>
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<td>MP3</td>
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<td>GND</td>
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</tr>
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</tr>
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<td>MP4</td>
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<td>GND</td>
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</tr>
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</tbody>
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</table>
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#### <ins>ETH EXP. connector</ins>
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505110-1692 connector
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Ethernet connector is routed to FMU through onboard switch.
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The onboard FMU is connected via the RMII bus with a speed of 100 Mbits.
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#### <ins>SD card connector</ins>
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MEM2085-00-115-00-A connector
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Connector for standard microSD memory card. This card is primarily used to store flight data and logs.
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## Other connectors
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### CAN 1, CAN 2 connectors
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The board contains two CAN buses - CAN1 and CAN 2. The buses support speeds up to 1 Mbits and in FD mode up to 8 Mbits.
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These connectors are not part of DCS2.Pilot board, but they are routed on DCS2.Adapter_board. This board (DCS2.Adapter_board) is fully modular and can be modified according to the customer's requirements. For more informations see: https://docs.airvolute.com/dronecore-autopilot/dcs2/adapter-extension-boards/dcs2.-adapter-default-v1.0/connectors-and-pinouts
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JST GH 1.25mm pitch, 4-Pin
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Matching connector JST GHR-04V-S.
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5V supply is limited to 1.9A by internal current limiter.
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<table border="1" class="docutils">
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<tbody>
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<tr>
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<th>Pin </th>
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<th>Signal </th>
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</tr>
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<tr>
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<td>1</td>
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<td>5V</td>
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</tr>
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<td>2</td>
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<td>CAN_H</td>
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</tr>
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<td>3</td>
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<td>CAN_L</td>
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</tr>
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<td>4</td>
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<td>GND</td>
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</tr>
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</tbody>
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</table>
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## UART Mapping
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- SERIAL0 -> USB (Default baud: 115200)
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- SERIAL1 -> UART1 (FMU SEC) (Default baud: 57600, Default protocol: Mavlink2 (2))
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- SERIAL2 -> UART2 (FMU SEC) (Default baud: 57600, Default protocol: Mavlink2 (2))
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- SERIAL3 -> UART3 (RX pin only labeled as PPM on PPM connector) (Since this is a secondary FMU, default protocol is set to NONE instead of RCIN (23))
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UARTs do not have RTS/CTS. UARTs 1 and 2 are routed to FMU_SEC. connector.
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## Loading Firmware
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Initial bootloader load is achievable only by SDW interface. Then it is possible to flash firmware thrugh onboard USB connection with Jetson host.
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