gX-200 GNSS/INS

MEMS-Based Inertial Navigation System

The gX-200 is a tactical-grade, MEMS-Based GNSS/INS unit, comprised of 9-DoF inertial sensors (3-axis accelerometers, 3-axis gyroscopes, & 3-axis magnetometer). Along with hi-performance, survey-grade multi-frequency/multi-constellations GNSS , and fused by a stable, powerful, Unscented-Kalman-Filter algorithm – which runs on Cortex-H7 floating-point double-precision processor at 480 MHz clock speed.

All these factors are fused together, to provide a PVT solution, along with quaternions, DCM matrix, attitude angle – and calibrated, compensated raw data.

 

Main Features

Roll/Pitch < 0.1⁰

Tactical-Grade Accelerometer < 1mg over Full Temp Range

Gyro Bias Stability 0.8 °/Hr

Low VRE < 100 µg/g2

Update Rate 1,000 Hz

Low Power Consumption 250 mA @ 12VDC

Rugged Design Mil-Spec Compliance

ITAR/MTCR-Free

Applications

Camera Gimbal

Tracking Antenna Systems

Optical Systems

Armored Vehicles

UAV/UGV

Target Acquisition systems

Radar North Finding system

Inertial Navigation (GNSS/INS)

Specifications

Magnetic2.0°
GNSS-Dynamic0.1°
Pitch/Roll
- Dynamic0.10°
- Static0.05°
Position - Horizontal1.5 m
SBAS< 0.5 m
RTK10 mm + 1ppm
Position - Vertical2.5 m
SBAS< 1 m
RTK1.5 cm + 1ppm
Velocity Accuracy< 0.03 m/sec (rms)
Output Rate1000 Hz
Latency< 5 msec
Receiver TypeMulti – Frequency / Multi – Constellations
1408 Channels
GPS L1/L2
Glonass L1/L2
SBAS
RTKBDS B1/B2
Galileo E1/E5b
QZSS L1/L5
Update Rate20 Hz
TTFFCold start < 30 sec
Warm start < 1 sec
RTK formatRTCM v2.3/3.0/3.2
Initialization Time< 5 sec
Velocity Accuracy0.03 m/sec (rms)
Time Accuracy20 ns (rms)
IMURaw Data & Compensated Gyro, Acc, Mag, Baro, Conning & Sculling
(ΔV ,ΔΘ)
GNSSUTC, Position, RTK
AttitudeRoll/Pitch/Yaw Quaternions, DCM, Euler
Inertial NavigationVelocity, Position, Attitude
AccelerometerGyroscopeMagnetometer
Full Scale Range± 10g ± 500° /sec | ± 4 Gauss
Bandwidth0…250Hz0…250 Hz0…50 Hz
Non Linearity0.2%< 0.05 % 0.1%
Bias
- Stability< 20 µg< 0.8 °/hr
- Repeatability ToTo± 300 µg< 20 °/hr
- Day-To-Day<400 µg< 15 °/hr
- One Year1500 µg
Over Full Temp<500 µg< 60 °/hr
Over 20 ° Span<150 µg< 20 °/hr
Hysteresis300 µg< 63 °/hr
- Repeatability500 ppm100 ppm
- over Temp100 ppm100 ppm
Random Walk0.02 m/sec/√Hr0.07 °/√Hr0
Resolution< 100 µg0.008 °/sec 1 mGauss
Noise density<20 µg /√Hz0.003 °/sec/√Hz 0300 nT RMS
Vibration Rectification<100 µg/g2 RMS<1°/hr/g
G-Sensitivity<10°/hr/g
Latency < 2 msec
MisAlignment<1 mRad2 mRad
Digital InterfaceRS232/RS422
Frame Rate1000 Hz Max
Peripherals2 x GPIO /// 1 x RS232
GPIO FunctionalityTrigger Input
Sync Out
PPS Out
Odometer
External GNSS
External Magnetometer
Air-Data
Start Up Time< 800 msec
Input Voltage9 VDC – 32 VDC
Power (incl. Antenna)360 mA @ 12VDC
ConnectorsPower/Data: Mini D-Type 21-pin
GNSS: SMA
Size80 x 66 x 56 mm
Weight<250 gr
Temp Operation-40° C to +71° C Mil-Spec 810-G Method 501.5 Procedure I
Shock500g, 3mSec ½ Sine Mil-Spec 810-G Method 516.6 Procedure V
Vibration12 G rms, 20-2000 Hz Mil-Spec 810-G Method 514.6 Category 17
Altitude70,000 feet Mil-Spec 810-G Method 500.5 Procedure III
PowerEN55022 Class A&B
EnclosureIP65 EN 595
MTBF50,000 Hours Mil-HDBK 217

DOCUMENTATION AND RESOURCES

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