High Heading Accuracy Inertial Navigation System with Mems Technology and Satellite Navigation

Product Details
Customization: Available
Output Signal Type: Digital Output
Measuring Shaft Quantities: Three
Manufacturer/Factory, Trading Company
Gold Member Since 2023

Suppliers with verified business licenses

Audited Supplier

Audited by an independent third-party inspection agency

Registered Capital
1000000 RMB
Plant Area
1001~2000 square meters
  • High Heading Accuracy Inertial Navigation System with Mems Technology and Satellite Navigation
  • High Heading Accuracy Inertial Navigation System with Mems Technology and Satellite Navigation
  • High Heading Accuracy Inertial Navigation System with Mems Technology and Satellite Navigation
  • High Heading Accuracy Inertial Navigation System with Mems Technology and Satellite Navigation
  • High Heading Accuracy Inertial Navigation System with Mems Technology and Satellite Navigation
  • High Heading Accuracy Inertial Navigation System with Mems Technology and Satellite Navigation
Find Similar Products
  • Overview
  • Product Description
  • Main Functions
  • Product Display
  • Product Parameters
  • Product Structure
  • Main Application Fields
  • Company Profile
Overview

Basic Info.

Model NO.
INS100C-B0
IP Rating
IP67
Certification
CE
Customized
Customized
Heading Accuracy
0.1deg
Attitude Accuracy
0.1deg (RMS)
Gyro Range
±450°/S
Gyro Zero Bias Stability
2°/H
Horizontal Velocity Accuracy
0.1m/S
Acc Range
±16g
Accelerometer Zero Bias Stability
30µg
Weight
≤0.4kg
Communication Interface
RS-422/RS-232/Can/Ethernet Interface/PPS
Voltage
9~36V
Power Consumption
≤10W
Mtbf
30000h
Vibration
5~2000Hz
Transport Package
Sponge and Box
Specification
117mm*96mm*39.8mm
Trademark
AVIC
Origin
China
Production Capacity
500/Month

Product Description

High Heading Accuracy Inertial Navigation System with MEMS Technology and Satellite Navigation

Product Description

 

The INS100C-B0 integrated navigation system consists of MEMS sensors and a high-end GNSS receiver board (NovAtel-718D), which is implemented through multi-sensor fusion and navigation solving algorithms. This product has high reliability and strong environmental adaptability. By matching different software, the product can be widely used in fields such as drones, unmanned vehicles, surveying and mapping, marine compasses, stable platforms, and underwater vehicles.

 

Main Functions

The integrated navigation system utilizes GNSS receiver to receive satellite navigation information for combined navigation, outputting carrier's pitch, roll, heading, position, velocity, time, etc.After losing the signal, it outputs the position, velocity and attitude information of inertial solution, and has a certain navigation accuracy maintenance function in a short time. When combined with navigation, it can output the raw information that can be used for post-processing to be processed by the IE post-processing software of NovAtel.

Product Display

High Heading Accuracy Inertial Navigation System with Mems Technology and Satellite Navigation
High Heading Accuracy Inertial Navigation System with Mems Technology and Satellite Navigation

 

Product Parameters

  
Project Indicators
Heading accuracy Dual GNSS (2m baseline) 0.1°(RMS)
Single GNSS 0.2°(RMS)
Post-processing 0.03°(RMS)
Course keeping (GNSS failure) 1°/min(RMS)
Attitude accuracy GNSS valid (single point L1/L2) 0.1°(RMS)
Inertia/odometer combination (optional) 0.1°(RMS)
Post-processing 0.02°(RMS)
Hold (GNSS failure) 1°/min(RMS)
Horizontal positioning accuracy GNSS valid, single point L1/L2 1.2m(RMS)
Inertia/odometer combination (optional) 2 ‰ D (D represents mileage, CEP)
RTK 2cm+1ppm(RMS)
Post-processing 1cm+1ppm(RMS)
GNSS failure 1m/10s,10m/30s,20m/60s(RMS)
Horizontal velocity accuracy GNSS valid, single point L1/L2 0.1m/s(RMS)
Inertia/odometer combination (optional) 0.1m/s(RMS)
Inertial/DVL combination (optional) 0.2m/s(RMS)
Gyroscope Measuring range ±450°/s
Zero bias stability 2°/h
Accelerometer Measuring range ±16g
Zero bias stability 30µg
Communication interface RS422 /RS232 Route 7
CAN (optional) Route 1
Baud rate up to 1Mbps
Transmitting frequency up to 200Hz
Ethernet interface 10M
Odometer differential input (optional) Route 2
PPS Route 1
EVENT Route 1
Electrical characteristics Voltage 9~36VDC
Power consumption ≤10W
Built-in memory (optional) 16G
Structural characteristics Size 117mm×96mm×39.8mm
Weight ≤0.4kg
Use environment Operating temperature -40ºC~+60ºC
Storage temperature -45ºC~+65ºC
Vibration 5~2000Hz,2g
Impact 30g,11ms
Reliability MTBF 30000h
Life span > 15 years
Continuous working time >24h

Product Structure

 

High Heading Accuracy Inertial Navigation System with Mems Technology and Satellite Navigation

Main Application Fields

High Heading Accuracy Inertial Navigation System with Mems Technology and Satellite Navigation
High Heading Accuracy Inertial Navigation System with Mems Technology and Satellite Navigation
High Heading Accuracy Inertial Navigation System with Mems Technology and Satellite Navigation
 

 

Company Profile


High Heading Accuracy Inertial Navigation System with Mems Technology and Satellite NavigationHigh Heading Accuracy Inertial Navigation System with Mems Technology and Satellite Navigation



 

Send your message to this supplier

*From:
*To:
*Message:

Enter between 20 to 4,000 characters.

This is not what you are looking for? Post a Sourcing Request Now
Contact Supplier