ANELLO AERIAL INS

High-Performance INS for Autonomous Aerial Operations In GPS-Denied Environments

INTRODUCTION

Equipped with three ANELLO Silicon Photonics Optical Gyroscopes (SiPhOG™), the ANELLO Aerial INS is redefining precision and reliability for navigation in demanding aerial environments. The ANELLO Aerial INS integrates the company's groundbreaking SiPhOG™ technology with its advanced sensor fusion engine to deliver unparalleled precision and reliability for drones, Unmanned Aerial Vehicles (UAVs), and Vertical Takeoff and Landing (VTOL) aircrafts.
Red rectangular device labeled ANELLO AERIAL INS with antennas and ports, featuring technical specifications and interface options listed around it, including bias instability, angle random walk, interfaces, GNSS-denied navigation, heading accuracy, IP68, and waterproof features.

KEY FEATURES

  • Reference-grade 100Hz position, velocity and attitude
  • 3-axis SiPhOG™ with < 0.5º/hr unaided heading drift
  • Dual triple-frequency GNSS receivers
  • Resilience in heavy shock and vibration environments
  • Highly accurate dead reckoning solution for GNSS-denied navigation
  • ANELLO AI Sensor Fusion Engine with GNSS spoofing detection
  • Compact and lightweight design with low power consumption < 6 W
  • IP68 – waterproof, resistant to corrosion, salt spray and chemicals

SPECIFICATIONS

Horizontal Position Accuracy1
SPS……………………………………………………………… 1.2 m rms
Velocity Accuracy…………………………………………………………… 0.03 m/s rms
Heading Accuracy2 …………………………………… 0.2° rms
Attitude Accuracy (Roll/Pitch) …………… 0.05° rms



Notes:
1. After Initialization
2. Properly Installed Antennae
IMU Performance
Optical Gyroscope (3-Axis)
Range………………………………………………………… +/-400°/s
Bias Instability……………………………………….< 0.5°/hr
Angle Random Walk……………………… < 0.05°/√hr
MEMS IMU (6-Axis)………………………………………… Accelerometer
Range……………………………………………………………………… 16g,
Bias Instability…………………………………………………… 10ug,
Random Walk…………………………………………………… 0.03m/s/√hr,
Gyroscope
up to 400°/s
1.5°/hr
0.3°/√hr
Optical Gyroscope (Heading/Z-Axis)
Range………………………………………………………… 200°/s
Bias Instability……………………………………….< 0.5°/hr
Angle Random Walk……………………… < 0.05°/√hr
MEMS IMU (6-Axis)………………………………………… Accelerometer / Gyroscope
Range……………………………………………………………………… 16g, up to 400°/s
Bias Instability…………………………………………………… 10ug, 1.5°/hr
Random Walk…………………………………………………… 0.03m/s/√hr, 0.3°/√hr
GNSS & Timing
Constellations……………………… GPS, GLONASS, Beidou, Galileo, QZSS, NavIC, SBAS, all L-band signals
PVT Output Data Rate …………………… up to 100 Hz
Synchronization…………………………………… PPS Out, PPS Sync In
Environment
Operating Temperature3 ………………….-10 to +50°C
Vibration ………………………………………………………… 5g rms
Shock Survival ………………………… 40g



Notes:
3. Option for +70 °C extended range upgrade
Electrical
Input Voltage …………………………………… 5 to 30 VDC
Power Consumption …………………… < 6 W typical
Digital Interface ………………. Ethernet, RS-232, RS-422, CAN
Physical
Size……………………………………. 4.4” x 3.4” x 1.9”
Weight……………………………. 0.75 lbs.