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Technical Specifications

Processor and Compute​

  • Real-time multicore microcontroller architecture
  • Dedicated processing resources for control loops, I/O handling, and system management
  • Hardware floating-point support for control algorithms

The compute architecture is optimized for deterministic flight control workloads rather than general-purpose computing.

Sensors​

  • Multiple inertial measurement units (IMUs) for redundancy
  • Integrated barometric pressure sensor
  • Independent sensor buses for fault isolation

Sensor selection and layout follow Pixhawk FMU v6x RT redundancy and reliability guidelines.

Power Requirements​

  • Supports regulated DC input within Pixhawk FMU v6x RT specifications
  • Separate internal power domains for logic, sensors, and I/O
  • Voltage and current monitoring support for battery failsafes

Power input should always be provided through approved power paths.

Environmental and Mechanical​

  • Designed for installation in vibration-prone UAV environments
  • Compatible with standard Pixhawk mounting patterns
  • Intended for use within typical UAV operating temperature ranges

Proper mechanical isolation and airflow improve long-term reliability.