Product overview
The makeflyeasy PixPilot V6 Pro is an autopilot for UAV applications including surveying, mapping and monitoring. Its hardware pairs an STM32H743 main processor with an STM32F103 coprocessor, housed in a CNC aircraft aluminum alloy shell measuring 94 × 49 × 23 mm and weighing 62 g. The integrated sensing configuration comprises one ICM-40605 and two ICM-42688-P acceleration and gyroscope sensors, plus two BMP388 barometers. Built-in vibration damping addresses mid-frequency and high-frequency vibration, while temperature compensation supports sensor operation.
Integration connections include five UART interfaces, two I²C interfaces, two CAN interfaces, 8+8 PWM channels, one SBUS output and one PPM/SBUS input, alongside a TF-Card slot and a Type-C connection. The autopilot supports simultaneous connection of two PMUs, GPS compass, airspeed meter and telemetry to form a dual redundant system. It monitors multiple sensor channels and switches redundantly upon a detected failure. Three power inputs provide over-voltage and low-voltage protection with priority-based automatic switching. Its operating temperature range is -10 °C to 55 °C.
Specifications
| Specification | Value & conditions |
|---|---|
| Product type | Makeflyeasy PixPilot V6 Pro professional-grade autopilot |
| Intended applications | Surveying, mapping and monitoring |
| Dual redundant system support | Supports a dual redundant autopilot systemWith two PMUs, GPS compass, airspeed meter and telemetry. |
| Vibration damping | Built-in damping targeting mid-frequency and high-frequency vibration |
| Sensor temperature compensation | Built-in high-precision temperature compensation system |
| Sensor redundancy switching | Real-time multi-channel sensor monitoring with automatic redundant switchingWhen a monitored sensor failure occurs. |
| Power input protection and switching | Three power inputs with over-voltage and low-voltage protection and priority-based automatic switching |
| Main processor | STM32H743 (32 Bit Arm Cortex-M7, 480Mhz, 2M Flash, 1M RAM) |
| Coprocessor | STM32F103 (32 Bit Arm Cortex-M3, 72Mhz, 64K Flash, 20K RAM) |
| Acceleration and gyroscope sensors | ICM-40605 ×1 and ICM-42688-P ×2, each providing acceleration and gyroscope sensing |
| Barometers | BMP388 ×2 |
| UART | 5 |
| I²C | 2 |
| CAN | 2 |
| PWM | 8+8 |
| SBUS-OUT | 1 |
| PPM/SBUS-IN | 1 |
| Power 1 | 2 |
| Power 2 | 2 |
| TF-Card slot | 1 |
| Type-C | 1 |
| Shell material | CNC aircraft aluminum alloy |
| Operating temperature | -10 °C to 55 °C |
| Dimensions | 94 × 49 × 23 mm |
| Weight | 62 g |
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