Key Design Points
Redundancy: 3x ICM-45686 IMU sensors (±32g) with BalancedGyro™ technology & 2x Barometer sensors
High performance STM32H753 Processor with clock speed up to 480 MHz
Modular flight controller: separated IMU, FMU, and Base system connected by a 100-pin & a 50-pin Pixhawk® Autopilot Bus connector.
Triple redundancy domains: Completely isolated sensor domains with separate buses and separate power control
All New advanced durable vibration isolation material with resonance frequency in the higher spectrum
Ethernet interface for high-speed mission computer integration
Temperature-controlled IMU board, allowing optimum working temperature of IMUs
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