logo
Products
PRODUCTS DETAILS
Home > Products >
Miniaturized High Accuracy Inertial Navigation System with Wide Operating Temperature -40~+85℃ for Automotive Applications
Products

Laser Inertial Navigation System

Fiber Optic Inertial Navigation System

Aircraft Inertial Navigation System

Marine Inertial Navigation System

Automotive Inertial Navigation System

AHRS System

IMU Inertial Measurement Unit

Fiber Optic Gyroscope

Ring Laser Gyroscope

Doppler Velocity Log

MEMS Inertial Navigation System
Contact Us
Miss. Yao
yao@inertial-systems.com
86--13212796772-18771004069
WeChat 13212796772
Contact Now
Miniaturized High Accuracy Inertial Navigation System with Wide Operating Temperature -40~+85℃ for Automotive Applications
  • name
  • name
  • name
  • name

Miniaturized High Accuracy Inertial Navigation System with Wide Operating Temperature -40~+85℃ for Automotive Applications

MOQ: 1
Price: 30000RMB
Standard Packaging: 30cm*30cm*28cm
Delivery Period: 14days
Payment Method: T/T
Supply Capacity: 50/1day
Details Information
Product Description
Detail Information
Place of Origin
WUHAN
Brand Name
CSSC
Certification
TRF250187465
Model Number
DP-MS1A
Weight:
≤150g,<80gram,<700g,≤80 Grams,56g
Operating Temperature:
-40~+85℃
Size:
65mm X 40mm X 18mm,150*110*50mm,Standard
Power Supply:
3.3V,5v Or 9~36v,DC +7V~+15VDC,18V DC- 36V DC
Screen Size:
10.1 Inch,30x40x3mm,9 Inch,5 Inch,no
Data Update Rate:
1000 Hz
Product Description
Miniaturized Inertial Navigation System - Automotive Grade
Key Functions
  • Supports initial alignment and system start-up under both static and dynamic conditions (e.g., swaying or disturbed)
  • Provides real-time output of navigation data, including position, heading, attitude, and velocity
  • Equipped with self-diagnostic capabilities and fault indication functions
Miniaturized Inertial Navigation System DP-MS 1A product image
Performance Specifications
Parameter (Typical Values) Unit DP-MS 1A
Gyroscope
Measurement Range°/s-
Bias Offset°/h15
Bias Instability (Allan Variance)°/h0.3
Bias Stability (10 s smoothing, 1σ, room temp)°/h3
Bias over Full Temperature Range°/h20
Bias Repeatability°/h3
Angle Random Walk°/√h0.15
Scale Factor Nonlinearityppm-
Scale Factor Repeatabilityppm-
BandwidthHz250
Cross Coupling%-
Accelerometer
Measurement Rangeg±80
Bias Stability (10 s smoothing, 1σ, room temp)mg1
Bias Variation over Temperaturemg0.5
Bias Repeatabilitymg5
Scale Factor Repeatabilityppm500
BandwidthHz100
Cross Coupling%0.1
System Specifications
Start-up Stabilization Times1
Data Update RateHz1000
Operating VoltageV5±0.5
Steady-state Power ConsumptionW1.5
Operating Temperature℃-45~80
Dimensionsmm44.8×38.6×20
Weightg52±5
Interface-RS-422
Tags: 

mems based inertial navigation system,  

mems inertial measurement unit,  

mems imu inertial navigation system

Recommended Products
Ultra-Low Noise MEMS Navigation System-Low-Power Consumption MEMS Measurement Unit

Ultra-Low Noise MEMS Navigation System-Low-Power Consumption MEMS Measurement Unit

Contact Now
Highly Integrated Micro Inertial Navigation Module-Real-Time Dynamic Attitude Measurement System

Highly Integrated Micro Inertial Navigation Module-Real-Time Dynamic Attitude Measurement System

Contact Now
Shock-Resistant High-Dynamic Inertial System-MEMS

Shock-Resistant High-Dynamic Inertial System-MEMS

Contact Now
High-Reliability Integrated Navigation System-Low-Power Consumption MEMS Measurement Unit

High-Reliability Integrated Navigation System-Low-Power Consumption MEMS Measurement Unit

Contact Now
High-Precision MEMS Navigation System

High-Precision MEMS Navigation System

Contact Now
MEMS Inertial Measurement Unit (MEMS-IMU)-Full Temperature Performance

MEMS Inertial Measurement Unit (MEMS-IMU)-Full Temperature Performance

Contact Now
Inertial Measurement Unit (IMU)-Bias Compensation

Inertial Measurement Unit (IMU)-Bias Compensation

Contact Now
Products
PRODUCTS DETAILS
Products

Laser Inertial Navigation System

Fiber Optic Inertial Navigation System

Aircraft Inertial Navigation System

Marine Inertial Navigation System

Automotive Inertial Navigation System

AHRS System

IMU Inertial Measurement Unit

Fiber Optic Gyroscope

Ring Laser Gyroscope

Doppler Velocity Log

MEMS Inertial Navigation System
Miniaturized High Accuracy Inertial Navigation System with Wide Operating Temperature -40~+85℃ for Automotive Applications
  • name
  • name
  • name
  • name
Miniaturized High Accuracy Inertial Navigation System with Wide Operating Temperature -40~+85℃ for Automotive Applications
MOQ: 1
Price: 30000RMB
Standard Packaging: 30cm*30cm*28cm
Delivery Period: 14days
Payment Method: T/T
Supply Capacity: 50/1day
Detail Information
Product Description
Detail Information
Place of Origin
WUHAN
Brand Name
CSSC
Certification
TRF250187465
Model Number
DP-MS1A
Weight:
≤150g,<80gram,<700g,≤80 Grams,56g
Operating Temperature:
-40~+85℃
Size:
65mm X 40mm X 18mm,150*110*50mm,Standard
Power Supply:
3.3V,5v Or 9~36v,DC +7V~+15VDC,18V DC- 36V DC
Screen Size:
10.1 Inch,30x40x3mm,9 Inch,5 Inch,no
Data Update Rate:
1000 Hz
Minimum Order Quantity:
1
Price:
30000RMB
Packaging Details:
30cm*30cm*28cm
Delivery Time:
14days
Payment Terms:
T/T
Supply Ability:
50/1day
Product Description
Miniaturized Inertial Navigation System - Automotive Grade
Key Functions
  • Supports initial alignment and system start-up under both static and dynamic conditions (e.g., swaying or disturbed)
  • Provides real-time output of navigation data, including position, heading, attitude, and velocity
  • Equipped with self-diagnostic capabilities and fault indication functions
Miniaturized Inertial Navigation System DP-MS 1A product image
Performance Specifications
Parameter (Typical Values) Unit DP-MS 1A
Gyroscope
Measurement Range°/s-
Bias Offset°/h15
Bias Instability (Allan Variance)°/h0.3
Bias Stability (10 s smoothing, 1σ, room temp)°/h3
Bias over Full Temperature Range°/h20
Bias Repeatability°/h3
Angle Random Walk°/√h0.15
Scale Factor Nonlinearityppm-
Scale Factor Repeatabilityppm-
BandwidthHz250
Cross Coupling%-
Accelerometer
Measurement Rangeg±80
Bias Stability (10 s smoothing, 1σ, room temp)mg1
Bias Variation over Temperaturemg0.5
Bias Repeatabilitymg5
Scale Factor Repeatabilityppm500
BandwidthHz100
Cross Coupling%0.1
System Specifications
Start-up Stabilization Times1
Data Update RateHz1000
Operating VoltageV5±0.5
Steady-state Power ConsumptionW1.5
Operating Temperature℃-45~80
Dimensionsmm44.8×38.6×20
Weightg52±5
Interface-RS-422
Tags: 

mems based inertial navigation system,

mems inertial measurement unit,

mems imu inertial navigation system

CSSC Star&Inertia Technology co.,ltd.
xiajia
Tel: 8613212796772
Sitemap |  Privacy Policy | China Good Quality Laser Inertial Navigation System Supplier. Copyright © 2025-2026 CSSC Star&Inertia Technology co.,ltd. . All Rights Reserved.