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AxisNav

Precision Navigation for Defense, Agriculture, and Maritime Unmanned Platforms.
100 % Made in India | AxisNav delivers high-reliability autonomous navigation solutions featuring rugged hardware, dual-redundant sensors and a multi-core processing architecture for mission-critical unmanned systems.
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aXISNAV THE iNDUSTRIAL UNMANNED BRAIN

Rugged Autopilot for Unmanned Systems

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System Overview

Hardware

  • Dual-Core Processor Architecture
  • Hard Real-Time Determinism
  • Dual Inertial Measurement Units
  • Dual Magnetometers
  • Dual Barometers
  • Integrated GNSS
  • Integrated Air speed sensor
  • Inbuild vibration protections
  • Data logging blackbox

Accuracy

  • Roll/Pitch: ~0.05
  • Heading: ~0.1
  • Position without RTK: ~2.5 m
  • Position with RTK: ~2.5 cm
  • Altitude: ~0.5 m
  • Horizontal velocity: ~0.1 m/s
  • Vertical velocity: ~0.1 m/s
  • Linear acceleration: ~0.1 mss
  • Anguler velocity: ~0.5 mss

Interfaces

  • 2 Telemtery port
  • 1 Spi port
  • 2 Uart port
  • 1 I2c port
  • 2 Can port
  • 16-Channel PWM output
  • 1 Usb port
  • 6-Channel adc inputs
  • 6-Channel io
  • 8-Channel RC inputs
  • 1 SBUS input

GCS

  • Designed for multiple platforms
  • Waypoint Navigation
  • Pattern Mapping
  • Zone mapping
  • Sensor Calibrations
  • multiple video feed
  • Input controls
  • Logging and simulation
  • Custom Peripherals
  • Firmaware Update
  • Pre-mission testings
  • Wide-view PFD with Video

Unmanned Systems

Autonomous Controller Compatibility

Hardware-level orientation and position stabilization engineered for unmanned aerial, maritime, and ground platforms requiring real-time sensor calibration.

Aviation

Multi-Rotor Drones

Dual-redundant 3-axis gyro stabilization for heavy-lift multi-rotor aerial platforms in aggressive turbulence.

Marine

Unmanned Surface Vessels

Maritime autonomous navigation control with multi-sensor fusion and wave-motion correction for unmanned surface craft.

Aviation

Autonomous Helicopters

Sub-degree Euler precision accuracy and dual-barometer altitude hold down to 0.5m for complex rotary-wing flight profiles.

Review Full GCS Specifications

Examine complete ground control system hardware components, pinouts, and dual-redundant multi-sensor fusion architectures in our technical wiki.

Access Technical Docs