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Update photos & diagrams for Pixhawk 6C Mini and 6X (#24687)
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@@ -9,31 +9,44 @@ _Pixhawk 6X_<sup>®</sup> is the latest update to the successful family of Pi
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It is based on the [Pixhawk® Autopilot FMUv6X Standard](https://github.com/pixhawk/Pixhawk-Standards/blob/master/DS-012%20Pixhawk%20Autopilot%20v6X%20Standard.pdf), [Autopilot Bus Standard](https://github.com/pixhawk/Pixhawk-Standards/blob/master/DS-010%20Pixhawk%20Autopilot%20Bus%20Standard.pdf), and [Connector Standard](https://github.com/pixhawk/Pixhawk-Standards/blob/master/DS-009%20Pixhawk%20Connector%20Standard.pdf).
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Equipped with a high performance H7 Processor, modular design, triple redundancy, temperature-controlled IMU board, isolated sensor domains, delivering incredible performance, reliability, and flexibility.
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Equipped with a high-performance H7 Processor, modular design, triple redundancy, temperature-controlled IMU board, and isolated sensor domains, delivering incredible performance, reliability, and flexibility.
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### Pixhawk 6X (Rev 3)
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### Pixhawk 6X (Rev 8)
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<img src="../../assets/flight_controller/pixhawk6x/pixhawk6x_hero_upright.png" width="230px" title="Pixhawk6X Upright Image" /> <img src="../../assets/flight_controller/pixhawk6x/pixhawk6x_exploded_diagram.png" width="400px" title="Pixhawk6X Exploded Image" />
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<img src="../../assets/flight_controller/pixhawk6x/HB_6X_rev8_V2A.png" width="420px"/><img src="../../assets/flight_controller/pixhawk6x/hb_6x_internal_v2.png" width="320px"/>
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#### Pixhawk 6X (Rev 3/4, discontinued)
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### Pixhawk 6X (ICM-45686)
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<img src="../../assets/flight_controller/pixhawk6x/pixhawk6x_hero_upright.png" width="150px" title="Pixhawk6X Upright Image" /> <img src="../../assets/flight_controller/pixhawk6x/pixhawk6x_exploded_diagram.png" width="280px" title="Pixhawk6X Exploded Image" />
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### Pixhawk 6X Baseboards Options
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:::: tabs
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::: tab Standard v2A
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:::
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::: tab Standard v2B
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:::
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::: tab Mini
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:::
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::: tab Jetson Baseboard
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:::
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::: tab CM4 Baseboard
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:::
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::::
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@@ -54,15 +67,15 @@ An independent LDO powers every sensor set with independent power control. A vib
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External sensor bus (SPI5) has two chip select lines and data-ready signals for additional sensors and payload with SPI-interface, and with an integrated Microchip Ethernet PHY, high-speed communication with mission computers via ethernet is now possible.
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The Pixhawk® 6X is perfect for developers at corporate research labs, startups, academics (research, professors, students), and commercial application.
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The Pixhawk® 6X is perfect for developers at corporate research labs, startups, academics (research, professors, students), and commercial applications.
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## Key Design Points
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- High performance STM32H753 Processor
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- High-performance STM32H753 Processor
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- Modular flight controller: separated IMU, FMU, and Base system connected by a 100-pin & a 50-pin Pixhawk® Autopilot Bus connector.
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- Redundancy: 3x IMU sensors & 2x Barometer sensors on separate buses
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- Triple redundancy domains: Completely isolated sensor domains with separate buses and separate power control
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- Newly designed vibration isolation system to filter out high frequency vibration and reduce noise to ensure accurate readings
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- Newly designed vibration isolation system to filter out high-frequency vibration and reduce noise to ensure accurate readings
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- Ethernet interface for high-speed mission computer integration
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- IMUs are temperature-controlled by onboard heating resistors, allowing optimum working temperature of IMUs 
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@@ -72,7 +85,11 @@ The Pixhawk® 6X is perfect for developers at corporate research labs, startu
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- 32 Bit Arm® Cortex®-M7, 480MHz, 2MB flash memory, 1MB RAM
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- IO Processor: STM32F100
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- 32 Bit Arm® Cortex®-M3, 24MHz, 8KB SRAM
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- On-board sensors
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- On-board sensors (Shipping Currently, Rev 8)
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- Accel/Gyro: 3x ICM-45686 (with BalancedGyro™ Technology)
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- Barometer: ICP20100 & BMP388
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- Mag: BMM150
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- On-board sensors (Rev 3/4, discontinued)
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- Accel/Gyro: ICM-20649 or BMI088
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- Accel/Gyro: ICM-42688-P
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- Accel/Gyro: ICM-42670-P
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@@ -182,14 +199,14 @@ The **POWER1** & **POWER2** ports on the Pixhawk 6X uses the 6 circuit [2.00mm P
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**Normal Operation Maximum Ratings**
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Under these conditions all power sources will be used in this order to power the system:
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Under these conditions, all power sources will be used in this order to power the system:
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1. **POWER1** and **POWER2** inputs (4.9V to 5.5V)
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1. **USB** input (4.75V to 5.25V)
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**Absolute Maximum Ratings**
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Under these conditions the system will not draw any power (will not be operational), but will remain intact.
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Under these conditions, the system will not draw any power (will not be operational) but will remain intact.
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1. **POWER1** and **POWER2** inputs (operational range 4.1V to 5.7V, 0V to 10V undamaged)
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1. **USB** input (operational range 4.1V to 5.7V, 0V to 6V undamaged)
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@@ -200,7 +217,7 @@ Under these conditions the system will not draw any power (will not be operation
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Digital I2C battery monitoring is enabled by default (see [Quickstart > Power](../assembly/quick_start_pixhawk6x.md#power)).
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::: info
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Analog battery monitoring via an ADC is not supported on this particular board, but may be supported in variations of this flight controller with a different baseboard.
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Analog battery monitoring via an ADC is not supported on this particular board but may be supported in variations of this flight controller with a different baseboard.
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:::
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## Building Firmware
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