Overview
CUAV X25 EVO is a high-reliability core controller for unmanned systems. It combines an STM32H7 (480 MHz, 2 MB Flash) processor with a triple industrial-grade IMU array, dual barometers, and RM3100 magnetometers. A redesigned power architecture supports 10–18 V input and provides up to 5 V/12 A external output to power heavy payloads. The controller integrates dual-path power redundancy, comprehensive ESD/over-current protection, RGB status indication, and a modular CORE/carrier design. It is compatible with ArduPilot and PX4, and suits multirotors, fixed-wing, VTOL, helicopters, UGV/USV/UUV and other platforms.
Key Features
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High-performance compute: STM32H7 @ 480 MHz, 2 MB Flash; low CPU usage headroom for advanced algorithms (non-GPS nav, FFT filters, LUA scripts).
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Industrial sensor suite:
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IMUs: 2× TDK IIM-42653 (±4000 °/s, ±32 g) + 1× TDK IIM-42652 (±2000 °/s, ±16 g).
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Magnetometers: PNI RM3100 (anti-interference).
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Barometers: TDK ICP20100 & Bosch BMP581 (dual).
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Heterogeneous IMU matrix with fault-tolerant switching.
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Dual-temperature-compensation system for the IMU: real-time compensation ±0.5 °C; vs. prior generation—15% lower temp drift, 25% better attitude solution consistency.
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Vibration isolation: 4th-gen inclined symmetric nylon matrix damping; optional external fixed-ear isolators to suppress abnormal high-frequency vibration and improve data fidelity.
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Power architecture: onboard 5 V/15 A high-power DC-DC; external port supports 5 V/12 A output; input range 10–18 V.
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Networking & buses: CAN bus (smart battery/ESC/servos, telemetry feedback) + 100 M Ethernet.
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Abundant I/O: up to 16 PWM via servo ports; up to 32 PWM through CAN expansion.
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Ruggedization & QA: dual-channel power redundancy, ESD & over-current protection, anti-static connector design, PCB conformal coating, and fully automated testing.
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RGB status indicator: multi-color LEDs for arming, power, GNSS/position, fault modes, etc.
Specifications
| Category | Detail |
|---|---|
| Processor | STM32H7 Arm® Cortex®-M7 @ 480 MHz, 2 MB Flash |
| Version | X25 EVO |
| IMUs | IIM-42653 ×2 (gyro ±4000 °/s; accel ±32 g); IIM-42652 ×1 (gyro ±2000 °/s; accel ±16 g) |
| Magnetometer | RM3100 |
| Barometers | TDK ICP20100 / Bosch BMP581 (dual) |
| PWM outputs | 16 (servo bank M1–M16) |
| Power inputs (CAN) | 2 |
| GPS ports | 2 |
| TELEM ports | 2 |
| UART4 | 1 |
| RC input | 1 (PPM / SBUS / DSM etc.) |
| DEBUG (DSU) | 1 |
| Ethernet | 1 (100 M) |
| CAN | CAN1 ×3, CAN2 ×2 (total 5) |
| SPI6 expansion | 1 |
| ADC | 1× 3V3, 1× 6V6 |
| USB | 1× Type-C |
| I²C | 3 |
| RSSI | 1 |
| Power module | PMU 2 Lite |
Operating Conditions & Physical
| Item | Value |
|---|---|
| Input voltage (controller) | 10–18 V |
| USB | 4.75–5.25 V |
| PMU 2 Lite supply range | 20–70 V |
| External 5 V rail | up to 12 A output (for peripherals/heavy payloads) |
| Operating temperature | −20 °C to +85 °C |
| Dimensions | 76.5 × 45.45 × 32.2 mm |
| Weight | 110 g |
Interfaces & Layout Highlights
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Dual POWER C1/C2 rails, RC IN, M1–M16 servo bank.
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Side connectors for UART/TELEM, ADC, USB-C (debug/IO), I²C, CAN1/CAN2, ETH.
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Designed CORE that can be detached for custom carrier board development.
Compatibility & Applications
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Firmware: fully compatible with ArduPilot and PX4 (drivers & features).
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Vehicles: multirotor, fixed-wing, VTOL, helicopters, UGV, USV, UUV/submersible, and other unmanned platforms.
In the Box (X25 EVO Kit)
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X25 EVO flight controller × 1
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CAN PMU2 Lite (15 V) power module × 1
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CAN expansion board × 1
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CAN data cables (35 cm) × 2
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USB Type-C cable (100 cm) × 1
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TELEM cables (30 cm) × 2
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RSSI cable (22 cm) × 1
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RC IN cable (30 cm) × 1
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CAN PMU2 Lite 15 V smart controller power cable (30 cm) × 1
Details


CUAV X25 EVO flight controller components labeled with chip models.




CUAV X25 EVO flight controller measures 76.5mm x 45.45mm, features debug, USB, and I2C3 ports, and includes four M2 screws for secure mounting.

X25 EVO Autopilot includes flight controller, power module, CAN expansion board, data and telemetry cables, Type-C cable, RSSI and RC IN wires, and power supply line.
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