AUTOPILOT SYSTEM

Z4 Autopilot

The Z4 Autopilot delivers stable flight and precise maneuvering with high-accuracy gyroscope and accelerometer sensors. It provides barometric altitude measurement, flight logging and GNSS-supported (GPS · GLONASS · Galileo) precise navigation.

14 PWM

Outputs (8 IO + 6 FMU)

5V / 400 mA

Average Consumption

GPS · GLONASS · Galileo

Multi-Constellation Support
Z4 Otopilot

Technical Specifications

Sensors

Gyroscope±450 °/sn
Accelerometer±2 / ±4 g
Barometer15 – 115 kPa
Operating Temperature-40°C / +85°C

Power & Connectivity

Power5 V · ~400 mA
PWM Outputs14 channels
CommunicationUART · I²C · CAN · SBUS/PPM
Navigation (GNSS)GPS · GLONASS · Galileo (2.5 m)

Key Capabilities

Stable and Precise Flight Control
Barometric Altitude Measurement
Flight Logging and Fault Analysis
Multi-Constellation (GNSS) Navigation
Rich Communication Interfaces
MILITARY AUTOPILOT

Z4 MIL Autopilot

The Z4 MIL is a modular, stackable autopilot / guidance computer developed for critical missions, featuring a military-grade IMU, isolated interfaces and MIL-STD-1553 support. It is compatible with PX4 and ArduPilot.

MIL-STD-1553

Military Data Bus

RTK GPS

Integrated Precise Positioning

9 – 36 V

Isolated Power Input

-40°C / +85°C

Operating Temperature
Z4 MIL Otopilot

Technical Specifications

Sensors

Gyroscope±450 °/sn
Accelerometer±2 / ±4 g
Magnetometer±800 µT
Operating Temperature-40°C / +85°C

Processor & Interfaces

ProcessorSTM32H7 + STM32F4
Interfaces7× RS422 · MIL-1553 · Ethernet · CAN · USB
PowerNominal 24 V (9–36 V) · 5 W
NavigationIntegrated RTK GPS

Key Capabilities

Modular and Stackable Structure (AI Module)
Galvanically Isolated Interfaces and Power Lines
MIL-STD-1553 Military Data Bus
Tactical / Strategic IMU Slot for INS
Use as a Guidance Computer
PX4 / ArduPilot Compatibility