This manual introduces the features of DJI XP3.1 autopilot, hardware system, control mode, system requirements, system framework, module introduction, system installation and debugging, outdoor test flight, flight precautions and other contents.
The DJI XP3.1 Standard is an autopilot system that combines GPS, a 6‑DOF inertial measurement unit, magnetometer and barometric altimeter to deliver precise flight control even when GPS signals are intermittent. It features dual‑MCU DSP+ARM processing, built‑in 16‑channel GPS receiver, MEMS gyroscope/accelerometer and a three‑axis magnetometer.
The manual covers system introduction, hardware installation, parameter tuning, flight testing procedures, and detailed safety checks. It includes wiring diagrams, mechanical drawings, a parts list, and instructions for compass calibration, fail‑safe setup, and mode selection (manual, self‑drive, attitude). This manual is written in Chinese.
| Hover accuracy (vertical) | ±1 m |
|---|---|
| Hover accuracy (horizontal) | ±2 m |
| Operating temperature | -10 °C ~ +70 °C |
| Operating voltage | 7.4~12 V DC |
| Recommended battery | Lithium, ≥2000 mAh, 7.4 V |
Use a lithium battery with at least 2000 mAh capacity and a nominal voltage of 7.4 V.
The system includes an integrated calibration program that allows users to perform both soft and hard magnetic calibration.
The remote must provide a fail‑safe function on the throttle (channel 1); other channels may not have fail‑safe capability.