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Resilient Navigation System

Overview
Resilient Navigation System is a low size, weight and power navigation system that combines GNSS, INS, anti-jammer and alternative navigation technologies to provide three layers of resilience for safe navigation.

Layer 1 GPSdome 1 - Industry’s only non-ITAR GPS anti-jammer. Ensures GPS availability during low power jamming conditions.
  • GPS L1 Protected frequency
  • 20 dB Attenuation
  • Low Size, Weight and Power
  • Low Latency
GPSdome 1 is a small-sized, add-on device that provides protection against GPS jamming, ensuring continuity of autonomous navigation and operation during jamming conditions. No other solution that offers the same protection is as small, light, affordable or as easily installed as GPSdome 1.

Layer 2 Honeywell Compact Inertial Navigation System - Combined GNSS and inertial navigation system for UAVs. Enables safe navigation for UAVsduring intermittent GNSS disruptions
  • Immune to intermittent GNSS outages <1 min
  • Integrated with Pixhawk
  • Tactical Grade Redundant inertial sensors
  • Easy Integration with navigation aiding systems
The Honeywell compact inertial navigation system (HCINS) for UAVs is a low size, weight and power (SWaP) inertial navigation system that is suitable for all types of UAVs. It enables safe navigation for UAVs during intermittent GNSS disruptions.

Layer 3 Honeywell Radar Velocity System - Range and velocity without GNSS. Enables safe navigation for UAVs during continuous GNSS disruptions.The Honeywell Radar Velocity System (HRVS) is a low size, weight and power (SWaP) millimeter radar-based navigation aiding system.Performs on all surfaces except still water.
  • 1-3% Distance traveled error when used with HCINS
  • Operational altitude 0-1 km
  • Performs on all surfaces except still water
  • Available in two variants 60 GHz | 80 GHz

Specifications

Dimensions

  • Length

    • 96mm
  • Width

    • 60mm
  • Depth

    • 28 mm
  • Weight

    • +22 grams (damping platform)
    • 115 grams (excluding damping platform)
  • Volume

    • 162cm³ cubic centimetre

Performance Data

  • Applications

    • Automotive Platforms
    • Drones
    • Robotics
  • Vibration

    • BFD Basic profile
  • Velocity errors X/Y/Z axes 9m/s

    • 0.04 m/s
  • Usually Bought With

    • GPSdome
    • HRVS (Honeywell Radar Velocity System)
  • Typical Performance

    • Attitude [deg] 0.04
    • Heading [deg] 0.28
    • Position Error [m] 2.5
    • Velocity Error [m/s] 0.04
  • Typical Heading Error with HCINS

    • 0.28 deg
  • Types of Products

    • IMU (MEMS)+GNSS Navigator
  • Time to First Fix

    • 35-60 sec
  • Software

    • Internal Software
  • Size

    • 96mm x 60mm x 28mm (excluding damping platform) millimetre
  • Signal Reacquisition

    • 2 sec
  • Shock

    • DO-160G; section 8, Category S, Curve C
  • Setup

    • Dual Atenna Setup
  • Output

    • Altitude
    • Attitude
    • Position
    • Velocity
  • Key Performance Variables

    • Altitude
    • Attitude
    • Position
    • Velocity
  • Features

    • Heading: 0.28 (deg)
    • MEMS based navigator
    • Position Error: 2.5 m (standalone)
  • Components

    • GNSS Antenna
    • GNSS Receiver
    • IMU
    • Processing Boards
  • Component of

    • Resilient Navigation
  • Communication Ports

    • Ethernet Communication
    • Serial Communication
  • Chassis Included

    • Yes, Plastic Chasis

 

  • Compatible Platform

    • Fixed Wing Drones
    • Multi-Copter Drones
    • Unmanned Aircraft
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