MICRO-MINIATURE INS

POLLUX-3

Inertial Navigation System

Highly compact MEMS-based Inertial Navigation System with Extended Kalman Filter (EKF) offering near-tactical performance. Provides precise positioning, velocity, attitude, and heading for UAVs, UGVs, and unmanned systems. Features integrated multi-constellation GNSS with 1.5m CEP position accuracy.

POLLUX-3 INS
40g
Weight
37mm
Compact Size
1.5m
CEP Accuracy
200Hz
Update Rate
0.1°
Roll/Pitch Accuracy
< 0.3°
Heading (GNSS)
< 1.5W
Power Consumption
MIL-STD
810G / 461E

Technical Specifications

Precision-engineered for mission-critical applications

Roll/Pitch Accuracy (Static)
0.1° (1σ)
Roll/Pitch Accuracy (Dynamic)
0.2° (1σ)
Heading Accuracy (GNSS)
< 0.3°
Heading Accuracy (Magnetometer)
< 1° (1σ)
Navigation Data Rate
200 Hz
IMU Data Rate
1000 Hz

Product Features

01

High Accuracy

<1.5m CEP position accuracy and 0.1 m/s(1σ) velocity accuracy with integrated multi-constellation GNSS for precision positioning of drones

02

Compact, Tiny SWAP

Tiny C-SWAP suitable for unmanned applications – Size: 37mm (L) x 37mm (W) x 15mm (H) and Power < 1.5W

03

Lightweight

Weighs just 40 grams, suitable for micro-UAV applications and yet ruggedized to meet tactical application requirements

04

Extended Kalman Filter

Advanced EKF algorithm providing best estimates of navigation parameters including position, velocities, attitude, and heading

Applications

Drone and UAV Navigation

Precision navigation and control for unmanned aerial vehicles with highly dynamic performance requirements

Autonomous Control and ADAS

Advanced driver assistance systems and autonomous navigation for ground vehicles and robotics

Ready to Deploy POLLUX-3?

Contact our defense solutions team for technical specifications, pricing, and integration support.