NP-FCC-H05

Product Details ​

Overview ​

NP-FCC-H05 is a high-performance, industrial-grade, integrated navigation and flight control product developed by the NextPilot team. It carries a high-performance, dual-redundant, built-in vibration-damped inertial measurement unit (IMU), offering high reliability, good stability and strong vibration resistance. It adopts self-developed navigation algorithms and loss-of-control protection strategies, delivering high positioning accuracy and strong anti-interference capability. It integrates powerful functions including moving-platform takeoff and landing, visual navigation and swarm formation flight, and provides external flight control interfaces for secondary development to meet application development needs across scenarios. The product suits 10 kg ~ 300 kg class UAV platforms of all types, including multirotor, fixed-wing, VTOL and tiltrotor, and paired with a professional ground station it delivers powerful flight functions and safe flight assurance.

Product Highlights ​

• Dual main processors, with separated flight control and navigation architecture
• Built-in high-performance IMU, installable without external damping
• Built-in high-performance navigation board
• Moving platform support
• Compliant with relevant GJB standards

Main Functions ​

The main functions of the navigation and flight control unit are:

• Supports multiple vehicle types, including multirotor, fixed-wing and VTOL;
• Multiple flight modes including manual, altitude hold, position hold, acro, loiter, mission, external control, autonomous takeoff and landing, and return to home;
• Emergency protection logic including data link loss protection, satellite signal loss protection, engine failure protection, and low voltage warning and protection;
• Remote takeoff and landing;
• Geofence;
• Hardware-in-the-loop and software-in-the-loop simulation;
• Multi-vehicle control;
• Multi-level formation support;
• Broad support for satellite navigation boards, including Novatel (OEM718D), Unicore (UM482, UM982) and others;
• High-precision industrial-grade IMU, no external damping required;
• Serial port firmware upgrade;
• Logging and replay (PX4 log format);
• Software version query.

Main Performance ​

Performance specifications of the navigation and flight control unit:

• Supply voltage: DC 9~36 V;
• Power consumption: < 12 W;
• Startup time: not more than 40 s;
• Altitude control accuracy: < 1 m;
• Serial ports: 8 channels;
• PWM: 16 channels;
• DO: 4 channels;
• ADC: 4 channels;
• Gyroscope: measurement range ±400 °/s, gyro bias 20 °/h (1σ);
• Accelerometer: measurement range ±10 g, accelerometer bias 1 mg;
• Operating temperature: -40 °C ~ 75 °C;
• Storage temperature: -45 °C ~ 80 °C;
• High and low temperature operation, vibration, shock and electromagnetic compatibility comply with GJB requirements.

Dimensions and Weight ​

• Dimensions: ≤ 112 mm × 72 mm × 42 mm (L × W × H);
• Weight: 400 g;
• Mounting hole diameter 4 mm, spacing 107 mm × 87 mm.

Included Accessories ​

The debug cable supplied with the navigation and flight control unit is shown below: