High Performance FOG and Quartz MEMS Inertial Sensors - Gyros, IMU, INS

EMCORE Corporation Visit Website

EMCORE is a leading provider of high-performance inertial navigation sensors and systems for aerospace, defense and commercial markets.

Our product suite utilizes Emcore’s state-of-the-art closed-loop Fiber Optic Gyroscope (FOG) sensor technology, along with recently acquired Systron Donner Inertial’s quartz MEMS inertial sensing solutions, to meet the demanding requirements of SWaP-conscious unmanned applications.

Our tactical and navigation grade gyroscopes, IMUs, and Inertial Navigation Systems (INS) are ideal for navigation, control and stabilization of UAVs (unmanned aerial vehicles), UGVs (unmanned ground vehicles) and AUVs/UUVs (unmanned underwater vehicles).

Fiber Optic Gyroscope (FOG) Sensors

EMCORE-Hawkeye™ EG-120 FOG

Ultra-compact, closed-loop gyroscope for demanding applications

EMCORE EG-120 Compact FOG for UAVsThe EG-120 FOG module is our smallest closed-loop FOG and the smallest, most affordable closed-loop FOG available on the market today. It features industry-leading SWaP characteristics and incorporates next-generation Field Programmable Gate Array (FPGA) electronics that deliver increased performance and reliability.

The EG-120 is an ideal solution for medium accuracy platform stabilization applications such as UAV weapons and camera systems. It is also available in a low power variant. Jump to specifications >

EMCORE-Hawkeye™ EG-200 FOG

Precision solid-state gyroscope for tactical grade applications

EMCORE EG-200 Tactical Solid-State FOGThe EG-200 is a tactical-grade FOG designed for high-accuracy navigation and low-noise line-of-sight stabilization applications. It features fully-integrated optics and Field Programmable Gate Array (FPGA) electronics, resulting in improved optical drift stability, higher linearity and greater environmental flexibility.

EG-200 units can be calibrated internally for better thermal effect, and have both digital and analog outputs, accommodating a wide variety of installation and interfacing parameters. Jump to specifications >

EMCORE-Hawkeye™ EG-1300 FOG

Low-noise gyroscope for navigational grade applicationsEMCORE EG-1300 Navigational Grade FOG

The EG-1300 is our lowest-noise FOG, ideal for precision navigation in GPS-denied environments – such as UUVs – as well as platform stabilization. Featuring advanced integrated optics and closed-loop FPGA design, it delivers higher accuracy, lower noise and greater efficiency in a low-SWaP package.

The EG-1300 can be calibrated internally for better thermal effect. In addition to providing both digital and analog outputs, the unit features separation of the electronics from the FOG’s sensing coil assembly, allowing for the most flexible installation and integration capabilities.

Comparison & Specifications:

EG-120
EMCORE EG-120 Compact FOG
EG-200
EMCORE EG-200 Tactical-Grade FOG
EG-1300
EMCORE EG-1300 Navigational Grade FOG
Dimensions2.36” D x 0.83”
(60mm x 21mm)
3.2” D x 0.8”
(81.2mm x 20.3mm)
Sensor: 3.6” D x 1.3”
(91.44mm x 33.02mm)
Electronics: 3.2” D x 0.8”
(81.2mm x 20.3mm)
Weight0.13 lbs (90g)14.5 oz (410g)
Bias
(Over Temperature)
≤1.0°/hr<0.8°/hr0.01°/hr
ARW/Noise≤0.04°/√ hr0.012°/√ hr0.001°/√ hr
Bandwidth300 Hz750 Hz500 Hz

Inertial Measurement Units (IMU)

EN-300 Inertial Measurement/Navigation Unit

Precision Three-Axis FOG IMU for UAVs

EMCORE EN-300 Series FOG IMUThe EN-300 is a higher-accuracy Fiber Optic Gyro-based IMU that is a form, fit and function compatible with a legacy equivalent, but with better performance needed for GPS denied navigation, precise targeting and line-of-sight stabilization. Applications include in inertial navigation for UAVs, dismounted soldiers, civilian unmanned aviation, and oil and gas exploration.

The low-noise, high-stability unit provides up to five-times better performance that competing system. It features internal signal processing that provides full stand-alone or aided navigation, with optional standard IMU delta velocity and delta theta outputs. With state-of-the-art FPGA electronics and sophisticated Kalman filtering, the unit is able to statically find North to less than one degree through gyro-compassing.

The EN-300 is available in three performance variants:

Specifications:

EN-300-1EN-300-3EN-300-5
Dimensions3.5” D x 3.35″
(89mm x 85mm)
Weight<1.7 lbs (770g)
Gyro Bias
(Over Temperature)
0.05°/hr0.1°/hr0.4°/hr
ARW/Gyro Noise0.005°/√ hr0.007°/√ hr0.03°/√ hr
Accelerometer Bias150 µg300 µg300 µg
Accelerometer Range30g (70g by request)

EMCORE-Orion™ Series Inertial Measurement Units

Ultra-high performance IMUs for UAVs, UUVs and UGVs

EMCORE-Orion Inertial Measurement Units (IMU)The EMCORE-Orion™ series of IMUs is designed for high-precision inertial measurement for unmanned vehicles such as UAVs, UUVs and UGVs. The state-of-the-art technology provides ultra-high performance while minimising Size, Weight and Power (SWaP) requirements.

Based around three-axis precision closed loop FOG technology, our proprietary FOG transceiver and next-generation FPGA electronics hardware, EMCORE-Orion™ IMUs are optimised for high-precision navigation applications and GPS-denied environments. Low noise and superior stability makes these IMUs ideal for the most demanding of unmanned systems inertial measurement requirements.

Specifications:

EN-1000iEN-2000i
Axes33
Accelerometer Axes33
Bias Stability (°/hr)0.0150.007
ARW/Noise (°/√ hr)0.0020.0008
Scale Factor (ppm)35<50
Max Acceleration (g)6060

Systron Donner Inertial SDI500 Tactical Grade IMU

Systron Donner InertialMEMS Quartz Inertial Measurement Unit

SDI500 Tactical Grade IMU Inertial Measurement UnitSDI500 is the first MEMS-based Inertial Measurement Unit (IMU) to demonstrate true tactical grade performance with 1°/hr bias stability and very low 0.02°/√hr angle random walk. SDI500 is rated for rugged military environments, with continuous Built-in Test (BIT), configurable communications protocols, electromagnetic interference (EMI) protection, flexible input power requirements and multiple output data formats.

Specifications:

GYRO CHANNELSACCELERATION CHANNELS
Bias1°/hr – 10°/hr1.0 mg – 2.0 mg
Bias in run Stability (typical)1.0°/hr – 2.0°/hr100 μg
Random Walk Noise0.02°/√hr – 0.03°/√hr100 μg /√Hz – 120 μg /√Hz
Operating Temperature-55°C to +85°C-55°C to +85°C
Vibration (Operating) 19g RMS 19g RMS

More information: SDI500 MEMS IMU

Inertial Navigation Systems (INS)

EMCORE-Orion™ Series Micro Inertial Navigation System (MINAV)

High-Precision Micro INS for GPS-Denied UAVs

EMCORE Orion Micro INS MINAVThe EMCORE-Orion™ series of high-precision Micro Inertial Navigation Systems (MINAV) is designed for unmanned vehicle navigation in GPS-denied environments, as well as accurate inertial measurement. The state-of-the-art technology provides navigation-grade performance close to that of a traditional RLG INS with 1/3 of the Size, Weight and Power (SWaP) requirements.

The low-noise, high-stability system incorporates our proprietary integrated electronics and optics devices, including a precision three-axis closed loop FOG, mechanical accelerometers and state-of-the-art FPGA electronics. The unit is able to be aided by an external GPS. In a GPS-denied environment the EN-1000 MINAV series will gyrocompass from approximately 0.8 to 1.2 milliradians depending on the model.

Specifications:

EN-1000EN-2000
Axes33
Position<1.5 nm/hr CEP<0.6 nm/hr CEP
Velocity (rms)<1.5 m/s (5 ft/sec)<0.6 m/s (2 ft/sec)
Heading (rms)<1.5 mrad (.08 deg)<0.8 mrad (.05 deg)
Pitch and Roll (rms)0.06 deg0.03 deg

Systron Donner Inertial – SDN500 GPS/INS

Systron Donner Inertial