Precision Inertial Sensors and Systems: IMU, GPS-INS, AHRS, MRU

Inertial Labs
Inertial Labs

Inertial Labs is a leading designer and manufacturer of position and orientation tracking systems for unmanned vehicles, based on the fusion of inertial sensors with a range of other cutting-edge sensing technologies. With our engineering expertise, we create high-performance inertial sensor systems with small size and low power requirements.

Our products are ideal for a variety of unmanned systems applications, including motion tracking, weapon orientation tracking, payload stabilization, and inertial position tracking for GPS-denied environments.

IMU-P Inertial Measurement Units (IMU)

High Performance Industrial & Tactical Grade IMUs

The IMU-P is a light-weight and compact high performance Inertial Measurement Unit (IMU), designed for a number of applications including UAV and AUV/ROV navigation and control.

The unit contains three highly accurate Advanced MEMS gyroscopes and three ultra high performance accelerometers for precise linear acceleration and angular rate measurements.

The IMU-P is an ITAR free inertial solution, that is fully calibrated and compensated over its operating temperature range. Both Industrial and Tactical grade units are available.

Compact size (39 x 45 x 22 mm) and low weight (70 gram) – ideal for integrated system applications.

IMU-P Inertial Measurement Unit for UAVs

IMU-P Industrial and Tactical Grade IMUs

Specifications

“Industrial” IMU-P “Tactical” IMU-P
Gyroscope Bias in-run Stability 3 deg/hr 1 deg/hr
Gyroscopes noise density 0.006 deg/sec√Hz 0.004 deg/sec√Hz
Accelerometer Bias in-run Stability 0.015 mg 0.005 mg
Accelerometers noise density 0.03 mg√Hz 0.025 mg√Hz
Pitch & Roll static accuracy 0.05 deg 0.05 deg
Power Consumption 0.8 @ 5V 0.8 @ 5V
Operating temperature -40 to +85 deg C -40 to +85 deg C

OS3D-FG Orientation Sensor

The OS3D-FG is a miniature Attitude and Heading Reference System designed for real-time orientation tracking applications. It fuses data from tri-axial MEMS gyroscopes, tri-axial MEMS accelerometers and tri-axial fluxgate magnetometers using an onboard Digital Signal Processor and state-of-the-art algorithms.

The OS3D-FG is ideal for a wide range of small unmanned vehicles, including UAVs, ROVs and ground robotics.

OS3D-FG UAV Orientation Sensor

Specifications

Size 45×16×14.5mm
Weight 12 grams
Power Consumption 0.15W
Output Data Rate up to 2000 Hz
Heading Accuracy 0.5 deg static, 1.5 deg dynamic
Attitude Accuracy 0.2 deg static, 0.7 deg dynamic
Gyroscope Bias in-run Stability 10 deg/hr
Accelerometer Bias in-run Stability 0.15 mg

More Information: OS3D-FG Orientation Sensor

AHRS-I Attitude and Heading Reference System

The AHRS-I is a high-accuracy Attitude and Heading Reference System that outputs absolute orientation (heading, pitch and roll) for both motionless and dynamic applications. It integrates precision 3-axis accelerometers, magnetometers and gyroscopes to provide absolute pitch and roll data, real time device rotation data and ongoing gyroscope corrections.

The AHRS-I utilizes our high-performance Fluxgate Magnetometer technology for superior stability and repeatability, making it an ideal solution for unmanned systems applications where superior accuracy is required.

AHRS-I UAV Attitude and Heading Reference System

Specifications

Size 90×27×26mm
Weight 73 grams
Output Data Rate up to 200 Hz
Heading Accuracy 0.4 deg static, 0.7 deg dynamic
Attitude Accuracy 0.1 deg static, 0.3 deg dynamic
Gyroscope Bias in-run Stability 10 deg/hr
Accelerometer Bias in-run Stability 0.005 mg
Magnetometer bias in-run stability 0.2 nT

AHRS-II Attitude and Heading Reference System

The AHRS-II is our family of next-generation Attitude and Heading Reference Systems featuring state-of-the-art algorithms for a wide range of dynamic motions of unmanned vehicles. Precision 3-axis accelerometers, magnetometers and gyroscopes provide heave, heading, pitch and roll data, as well as high-frequency real time device rotation data and ongoing gyroscope corrections.

The AHRS-II is available in three different models – Basic, Enhanced and Professional – to provide desired levels of accuracy and stability for all your unmanned systems applications.

AHRS-II Attitude and Heading Reference System

Specifications

Model AHRS-11-B (Basic) AHRS-11-E (Enhanced) AHRS-11-P (Professional)
Size 120 x 50 x 53 mm 120 x 50 x 53 mm 120 x 50 x 53 mm
Weight 220g 220g 220g
Heading Accuracy
(static | dynamic)
1 deg | 1.5 deg 1 deg | 1.5 deg 0.3 deg | 0.6 deg
Pitch & Roll Accuracy
(static | dynamic)
0.2 deg | 0.5 deg 0.1 deg | 0.3 deg 0.1 deg | 0.3 deg
Gyroscope Bias in-run Stability 1 deg/hr 1 deg/hr 1 deg/hr
Accelerometer Bias in-run Stability 0.02 mg 0.005 mg 0.005 mg
Magnetometer Bias in-run Stability 4 nT 4 nT 0.2 nT

GPS-Aided Inertial Navigation Systems

Our family of GPS-Aided Inertial Navigation Systems combines support for multi-GNSS constellation signals (L1 & L2 GPS, GLONASS, GALILEO and BEIDOU) with state-of-the-art 3-axis accelerometers, magnetometers and gyroscopes to provide accurate position, velocity, heave and absolute orientation data for both unmanned aircraft and ground robotics.

Three different models of INS are available – Basic, Professional and Dual Antenna – to provide desired levels of accuracy and stability for your particular unmanned systems application.

UAV GPS-Aided Inertial Navigation Systems

Specifications

 INS-B Inertial Navigation System  INS-B Inertial Navigation System  INS-D Inertial Navigation System
Model INS-B (Basic) INS-P (Professional) IND-D (Dual Antenna)
Size 120 x 50 x 53 mm 120 x 50 x 53 mm 120 x 50 x 53 mm
Weight 220g 280g 320g
Position Accuracy 1.5 m (GPS L1)
1.2 m (GPS L1&L2)
0.6 m (SBAS)
0.4 m (DGPS)
0.05 m (PP)
0.01 m + 1 ppm (RTK)
1.5 m (GPS L1)
1.2 m (GPS L1&L2)
0.6 m (SBAS)
0.4 m (DGPS)
0.05 m (PP)
0.01 m + 1 ppm (RTK)
1.5 m (GPS L1)
1.2 m (GPS L1&L2)
0.6 m (SBAS)
0.4 m (DGPS)
0.05 m (PP)
0.01 m + 1 ppm (RTK)
Heading Accuracy
(static | dynamic)
1 deg | 0.1 deg 0.4 deg | 0.1 deg 0.08 deg | 0.08 deg
(2m baseline)
Velocity Accuracy 0.03 m/sec 0.03 m/sec 0.03 m/sec
Pitch & Roll Accuracy
(dynamic)
0.1 deg 0.1 deg 0.1 deg
Gyroscope Bias in-run Stability 1 deg/hr 1 deg/hr 1 deg/hr
Accelerometer Bias in-run Stability 0.005 mg 0.005 mg 0.005 mg

Motion Reference Units (MRU)

Our Motion Reference Units are high-performance strapdown motion sensors specifically designed for marine applications such as ROVs. Utilizing precision solid state 3-axis accelerometers, magnetometers, gyroscopes and barometric sensors, the units output highly accurate position, velocity, acceleration, heading, pitch & roll, and heave, sway & surge data.

The Motion Reference Units are available in three different models – Basic, Enhanced and Professional – to provide desired levels of accuracy and stability as well as the required outputs for your particular application.

Motion Reference Units

Video: MRU Qualification Tests

Model Comparison: Measured Parameters

 MRU-B UAV Motion Reference Unit  MRU-B UAV Motion Reference Unit  MRU-P UAV Motion Reference Unit
Model MRU-B (Basic) MRU-E (Enhanced) MRU-P (Professional)
Heave (% / cm)
Pitch & Roll (deg)
Heading / Yaw (deg)
Velocity (meters / sec)
DGPS / RTK Positions (meters)

Specifications

Model MRU-B (Basic) MRU-E (Enhanced) MRU-P (Professional)
Size 120 x 50 x 53 mm 120 x 50 x 53 mm 120 x 50 x 53 mm
Weight 220g 280g 320g
Position Accuracy N/A N/A 0.01 m + 1 ppm (RTK)
Heave accuracy 5% / 5cm 5% / 5cm 5% / 5cm
Heading Accuracy
(static | dynamic)
N/A 0.6 deg | 0.1 deg 0.4 deg | 0.1 deg
Velocity Accuracy N/A N/A 0.03 m/sec
Pitch & Roll Accuracy
(dynamic)
0.08 deg | 0.03 deg 0.08 deg | 0.03 deg 0.08 deg | 0.03 deg
Gyroscope Bias in-run Stability 1 deg/hr 1 deg/hr 1 deg/hr
Accelerometer Bias in-run Stability 0.005 mg 0.005 mg 0.005 mg

More Information: Motion Reference Units

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