ITILaboratory / INS-GNSS Navigation

AINSGS2

A high-precision inertial-satellite navigation system for autonomous, transport, aviation, marine and special platforms.

Request integrationTechnical specifications
8 IMU1000 Hz INS9-36 V DC
AINSGS2 device
Modular navigation platform with redundant sensors, Ethernet Web UI, CAN FD, UART and PPS synchronization.

Purpose

Navigation, control and telemetry in one device

AINSGS2 combines synchronized IMUs, GNSS, barometer, magnetometer, EKF filtering, service telemetry and a web interface. The system remains operational under vibration, high dynamic loads and temporary GNSS loss.

Key advantages

Architecture for mission-critical platforms

Measurement redundancy

8 synchronized IMUs improve motion estimation and reduce the effect of individual channel failures.

INS/GNSS Fusion

EKF filtering, Dead Reckoning and modern GNSS support for stable navigation.

Fast telemetry

INS update rate up to 1000 Hz for dynamic platforms, autopilots and control loops.

Industrial interfaces

Ethernet, CAN FD, UART, SPI, I2C and PPS for system integration.

Web monitoring

Configuration, diagnostics, calibration and parameter control through Web UI.

Data protection

Safe Save on power loss, state control and protection of critical settings.

Applications

Platform for air, ground and marine carriers

UAVUAV and UAS
Ground platformGround platforms
Surface vesselSurface vessels
SubmersibleSubmersibles
Autonomous platformAutonomous platforms
Mobile mappingMobile mapping
Civil aviationCivil aviation
Military aviationMilitary aviation

Technical specifications

Core AINSGS2 parameters

ProcessorSTM32H755ZI, Cortex-M7 + Cortex-M4
IMU8 x TDK ICM-45686, 6-axis
Accelerometer±2 g ... ±32 g
Gyroscopeup to ±4000 °/s
INS rateup to 1000 Hz
GNSSu-blox M10, GPS/Galileo/BeiDou/GLONASS/QZSS/SBAS
SensorsRM3100 magnetometer, SPL06-001 barometer
InterfacesEthernet, CAN FD, UART, SPI, I2C, PPS
Power9-36 V DC
Temperature-40 ... +85 °C
Size120 x 90 x 45 mm, mass up to 450 g
AINSGS2 dimensions
Compact enclosure for mobile and onboard platforms.

Comparison

AINSGS2 among comparable navigation systems

SystemClassIMUINS rate, HzNavigation during GNSS loss
Pixhawk Cube OrangeAHRS/GNSS1400up to 10-30 s
VectorNav VN-100Tactical AHRS11000up to 1-5 min
VectorNav VN-300INS/GNSS11000up to 30 min
SBG Ellipse-NINS/GNSS2-4200up to 60 min*
Advanced Navigation SpatialINS/GNSS2-4200up to 60 min*
AINSGS2INS/GNSS81000up to 2 h+

* Values depend on operating conditions and system configuration.

Interfaces

Connection to control and diagnostic systems

AINSGS2 interfaces
ETH, CAN, UART and PPS are routed to dedicated connectors.

Ethernet

Web UI, API, firmware update and fast service access.

CAN FD

Data exchange with autopilot, controller or vehicle system.

UART

GNSS MSP, service telemetry and integration channels.

PPS IN/OUT

Synchronization of sensors, external systems and timestamps.

Reliability

Operation in demanding conditions

AINSGS2 is built for systems where data stability, state control and predictable integration are critical. Special versions can be configured for high loads, high-altitude use and autonomous navigation.

Safe SaveDead ReckoningRTK readyPPS sync

Contacts

We will prepare a configuration for your platform

Describe the carrier, interfaces, data rate, operating environment and navigation requirements.

Contact us