ANELLO EVALUATION KIT

INTRODUCTION

Powered by ANELLO's Sensor Fusion Engine and unique optical gyroscope technology, the ANELLO Photonics Optical Gyroscope & GNSS/INS EVALUATION KIT (EVK) can maintain centimeter accuracy in conditions where far more expensive reference-grade systems degrade, including extended full GNSS loss operation. Unlike other positioning and localization systems, the ANELLO EVK is more stable over wide temperature ranges and under extreme vibration due to its unique optical gyroscope solution.
THE ANELLO EVK INERTIAL NAVIGATION IS PERFECT FOR MAPPING, SURVEYING, ROBOTICS, CONSTRUCTION, TRUCKING,
AGRICULTURE, DEFENSE, AEROSPACE AND AUTONOMOUS VEHICLE APPLICATIONS.
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THE ANELLO GNSS/INS EVALUATION KIT INCLUDES EVERYTHING TO GET STARTED:
INS, TWO DUAL-BAND GNSS ANTENNAE, AND CABLES

NAVIGATE THE IMPOSSIBLE WITH THE ANELLO EVALUATION KIT

Dead Reckoning in GNSS-Denied Environments

Testing The ANELLO EVK in Urban Canyon

KEY FEATURES

  • Reference-grade 100 Hz Position, Velocity, and Attitude
  • < 0.5º/Hr Unaided Heading Drift
  • Accurate in severe multipath and GNSS denied
  • Dual 184-channel five constellation dual-band GNSS receivers
  • GPS, Glonass, Galileo, Beidou (Compass), QZSS
  • Reliable Autonomous Land Vehicles, Advanced ADAS Systems
  • Precise Heavy Equipment and Machine Control
  • Convenient and Fast Setup

SPECIFICATIONS

Horizontal Position Accuracy
SPS………………………………………………………………1.2 m cep
RTK2……………………………………………………………0.02 m cep
60s GNSS Outage3…………………………< 1.0 m rms
Velocity Accuracy…………………………………………0.01 m/s rms
Heading Accuracy4………………………………………0.2° rms
Attitude Accuracy (Roll/Pitch)………………0.02° rms



Notes:
1. After Initialization
2. < 20km Baseline from Base
3. Additional Drift Post GNSS Loss, with Wheel Speed Aiding
4. Properly Installed Antennae
IMU Performance
Optical Gyroscope (Heading/Z-Axis)
Range………………………………………………………… 200°/s
Bias Instability……………………………………….< 0.5°/hr
Angle Random Walk……………………… < 0.05°/√hr
MEMS IMU (6-Axis)…………………………… Accelerometer
Range………………………………………………………… 8g
Bias Instability……………………………………… 20ug
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………………………………………………………………………….8g, up to 400°/s
Bias Instability…………………………………………………… 20ug, 1.5°/hr
Random Walk…………………………………………………………0.03m/s/√hr, 0.3°/√hr
GNSS & Timing
Signal Bands……………………… L1 C/A, L2C, L1OF, L2OF, B1I, B2I, E1, E5b and SBAS
RTK Initialization Time…. <1 min, using RTCM3 corrections
Output Data Rate…………………… GPS: 4 Hz, IMU: 200 Hz, INS: 100 Hz
Environment
Operating Temperature ………………….-40 to +70°C
Vibration ………………………………………………………… IEC 60068-2-6 (5g)
Shock Survival ………………………… MIL-STD-810G (40g)
Electrical
Input Voltage …………………………………… 8 to 30 Vdc
Power Consumption …………………… 4 W typical
Digital Interface ………………. Ethernet, USB C
Physical
Size……………………………………. 4.2” x 1.5” x 5.0”
Weight……………………………. 1 lbs.

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