ArianNav GPS/INS - Aeroart Technology

ArianNav GPS/INS - Aeroart Technology
INERTIAL MEASUREMENT UNIT /
ATTITUDE HEADING REFERENCE SYSTEM
Embedded Navigation Solutions
ArianNav GPS/INS
High-Performance Embedded Navigation
PRODUCT OVERVIEW
HIGHLIGHTS
The ArianNav is a miniature, light weight, low power, high-perfor-
On-board Extended Kalman filter running at 50 Hz,
mance Inertial Measurement Unit (IMU) and Attitude and Head-
IMU Data available at 200Hz
ing Reference System (AHRS) available in a surface mount pack-
Continuous attitude solution over the complete 360° range
age or aluminum encased Rugged module. Incorporating the
of motion
latest in MEMS technology, the ArianNav combines 3-axis
Static accuracy better than 0.5° in pitch/roll, 2° in heading
accelerometers, gyros, magnetometers, barometric pressure sensor,
Individually calibrated for bias, scale factor, misalignment,
dynamic pressure sensor and a 32-bit microprocessor into an
& gyro g-sensitivity
extremely compact design.
Available with standard (at +25°C) or full temperature
The ArianNav computes and outputs a real-time, drift-free attitude
solution (i.e. 3D orientation) that is continuous over a complete
range of 360° motion. All ArianNav sensors go through a rigorous
calibration process at the ArianNav production facility to ensure
compensation (-40°C to +70°C)
On-line accelerometers & gyros bias
estimation
On-line data recording on Micro SD card
the highest quality inertial measurements and attitude estimates.
The small size, high performance, and cost-effectiveness of the
ArianNav provides unprecedented opportunities for embedded
FEATURES
navigation.
Vector Processing Engine (VPE) 1.0 Toolboxes
Real-time magnetic & acceleration disturbance rejection
Adaptive signal filtering
Dynamic filter tuning
On-board Hard compensation
User configurable messages using simple ArianNav protocol
On-board World Magnetic and Gravity Reference Models
On-board gyro drift compensation
Multi-sensor synchronization
Dynamic and barometric pressure
sensor
T :+989386258614
www.Aeroart.ir
[email protected]
VN-100 Dev DEVELOPMENT KITS
TECHNICAL SPECIFICATIONS
Attitude & Heading
Range (Heading/Roll):
Range (Pitch):
1
Static Accuracy (Heading, Magnetic):
Static Accuracy (Pitch/Roll):
Dynamic Accuracy (Heading, Magnetic):
Dynamic Accuracy (Pitch/Roll):
Angular Resolution:
Repeatability:
Output Rate:
Position
Output Type
Accuracy SEP2
Resolution
±180 °
±90 °
2.0 ° RMS
0.5 ° RMS
2.0 ° RMS
1.0 ° RMS
< 0.05 °
< 0.2°
50 Hz
User configurable, ECEF or geodetic
5m
0.03m
ArianNav Rugged Development Kit
• USB & Serial Adapter Cables
• Cable Connection Tool
• Carrying Case
• Software Development Kit
Gyro
Output Rate:
Range:
In-Run Bias Stability:3
Linearity:
Noise Density:
Bandwidth:
Alignment Error:
±250 °/s
< 1 °/s
< 0.1 % FS
0.0035 °/s /√Hz
256 Hz
±0.1 °
Accelerometer
Range:
In-Run Bias Stability:
Linearity:
Noise Density:
Bandwidth:
Alignment Error:
±16 g
< 0.04 mg
< 0.5 % FS
0.14 mg/√Hz
260 Hz
±0.1 °
Magnetometer
Range:
Linearity:
Noise Density:
Bandwidth:
Alignment Error:
±12 Gauss
< 0.1 %
140 µGauss/√Hz
50 Hz
±0.1 °
Pressure Sensors
Static pressure
Range:
Resolution:
Accuracy:
Error Band:
Bandwidth:
Dynamic pressure
Range:
Resolution:
APPLICATIONS
0-10kpa(0-130m/s sea level)
3 Pa
Environment
Operating Temp:
Storage Temp:
-40°C to +70°C
-40°C to +70°C
Electrical:
Input Voltage:
Current Draw:
Max Power
Consumption:
Digital Interface:
7.5 V to 12.4 V
50 mA @ 7.5 V
375 mW
Serial TTL, RS-232
Physical:
Size:
Weight:
Interface:
108 x 65 x 30 mm
210 g
9-pin DB9
Operation Limits:
Altitude:
Speed:
1
2
3
UAVs, UAS, Manned Aircraft
Robotics
ROVs
Smart Weapons
100 to 1200 mbar
0.042 mbar
±1.5 mbar
±2.5 mbar
50 Hz
50000 m
500 m/s
DEVELOPMENT TOOLS
Inertia link GUI: Powerful and user-friendly GUI allows you to display
sensor output as a 3D object, graph inertial data, configure sensor
settings, perform data-logging, & more.
Software Development Kit: Interface via C/C++, .NET & MATLAB development environments.
Engineering Support: Dedicated and responsive engineering support
team with combined experience in sensing, guidance, navigation, and
controls.
Custom Solutions Available: Application-specific modeling & algorithm
development; controls & closed-loop navigation solutions; custom
form-factors & packaging; integration with other external sensors;
displays, GUIs & other software packages; tailored calibrations;
custom communication protocols.
With proper magnetic declination, suitable magnetic environment
and valid hard/soft iron calibration.
Position accuracy when GPS solution is available, given as spherical
error probable. In case of temporary GPS outage, position accuracy is
subject to velocity random walk
Angular rate biases are consistently removed when GPS solution is
available and the vehicle is accelerating.
© 2016 ArianNav Technologies, LLC. All rights reserved.
Specifications subject to change without notice. Version 12-0002-R3
www.Aeroart.ir
[email protected]
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