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High-Precision Laser Gyro Inertial Navigation System for Marine and Aviation Guidance

High-Precision Laser Gyro Inertial Navigation System for Marine and Aviation Guidance

MOQ: 1 SET
Ceny: $1000-$100000
Okres dostawy: 30 dni roboczych
metoda płatności: T/T
Pojemność dostaw: 100 zestawów rocznie
Szczegółowe informacje
Miejsce pochodzenia
Chiny
Nazwa handlowa
Star & Inertia Technology
Numer modelu
Dubhe-500
Podkreślić:

integrated strapdown inertial navigation system

,

OEM strapdown inertial navigation system

,

RLG ins gyro

Opis produktu

Product Description

The laser gyro inertial navigation system uses laser gyroscopes and quartz accelerometers as its core sensing elements. With strapdown architecture and real-time navigation algorithms, it ensures high accuracy and stable navigation performance. The system supports multiple operation modes, including hybrid inertial/satellite navigation and standalone inertial navigation, providing continuous heading, attitude, velocity, and position data for marine and aviation platforms.


This solution is positioned as a good quality guidance INS guidance system for both maritime and aviation users. As a guidance INS guidance system provider and manufacturer, the product line offers reliable standalone INS options and ruggedized configurations for harsh environments. The market includes global guidance INS guidance system suppliers and integrators, with competitive guidance INS guidance system price levels depending on configuration and platform requirements.


For aerospace customers, guidance INS system aviation companies seek stable and precise attitude data, while maritime operators value dependable positioning under satellite signal loss. The unit is also available for guidance INS guidance system sales, supporting OEM and system integration demands across different markets.


Key Advantages

  • High-precision laser gyro INS guidance system
  • Real-time attitude and positioning output
  • Supports inertial/GNSS integrated operation
  • Ruggedized structure for marine and aviation environments
  • Reliable standalone INS performance during GNSS outage
  • Compatible with shipborne, airborne, and unmanned platforms


Application Markets

  • Maritime navigation & ship guidance
  • Survey and offshore engineering vessels
  • Defense and coast guard platforms
  • Aviation guidance and attitude control
  • UAV / USV / UUV inertial guidance
  • Industrial and research institutions


Series Maritime Inertial Navigation System(INS-M)
Type Dubhe-M48
Accelerometer Months Bias Repeatability() 10μg
Months Scale Factor Accuracy() ≤10ppm
Gyro Bias Repeatability() 0.01°/hr
Scale Factor Accuracy() 10ppm
Random walk() 0.003°/hr
Features Angular Rate ≥±400°/sec
Angular Acceleration 100000°/sec2
Acceleration 25g
Speed accuracy(Pure inertia) 0.6kn,RMS
Speed accuracy(GNSS combination) 0.4kn,RMS
Angular Attitude  Any Orientation
Startup time ≤10sec
Input/output 3 RS422 full-duplex serial ports, 1 100M Ethernet port
Alignment time 1hr
Position accuracy Pure inertia 1nm/48h,CEP
INS/DVL Combination 0.3%D,RMS
INS/GNSS Combination better than satellite accuracy
Heading Accuracy Pure inertia 0.04°sec(L),RMS
INS/GNSS combination 0.02°,RMS
Pitch & Roll Accuracy Pure inertia 0.02°,RMS
INS/GNSS combination 0.01°,RMS
Characteristics Power consumption 40W
Dimensions(Lmm×Wmm×Hmm) 232×186×160
Weight 8.2kg
Temperature  -40~60
Shock 15g,Half-sine wave 11ms
Input Voltage DC24V(±25%)
cooling Conduction to mounting plate
Vibration  20~2000Hz,6.06g
MTBF 10000 hours


produkty
szczegółowe informacje o produktach
High-Precision Laser Gyro Inertial Navigation System for Marine and Aviation Guidance
MOQ: 1 SET
Ceny: $1000-$100000
Okres dostawy: 30 dni roboczych
metoda płatności: T/T
Pojemność dostaw: 100 zestawów rocznie
Szczegółowe informacje
Miejsce pochodzenia
Chiny
Nazwa handlowa
Star & Inertia Technology
Numer modelu
Dubhe-500
Minimalne zamówienie:
1 SET
Cena:
$1000-$100000
Czas dostawy:
30 dni roboczych
Zasady płatności:
T/T
Możliwość Supply:
100 zestawów rocznie
Podkreślić

integrated strapdown inertial navigation system

,

OEM strapdown inertial navigation system

,

RLG ins gyro

Opis produktu

Product Description

The laser gyro inertial navigation system uses laser gyroscopes and quartz accelerometers as its core sensing elements. With strapdown architecture and real-time navigation algorithms, it ensures high accuracy and stable navigation performance. The system supports multiple operation modes, including hybrid inertial/satellite navigation and standalone inertial navigation, providing continuous heading, attitude, velocity, and position data for marine and aviation platforms.


This solution is positioned as a good quality guidance INS guidance system for both maritime and aviation users. As a guidance INS guidance system provider and manufacturer, the product line offers reliable standalone INS options and ruggedized configurations for harsh environments. The market includes global guidance INS guidance system suppliers and integrators, with competitive guidance INS guidance system price levels depending on configuration and platform requirements.


For aerospace customers, guidance INS system aviation companies seek stable and precise attitude data, while maritime operators value dependable positioning under satellite signal loss. The unit is also available for guidance INS guidance system sales, supporting OEM and system integration demands across different markets.


Key Advantages

  • High-precision laser gyro INS guidance system
  • Real-time attitude and positioning output
  • Supports inertial/GNSS integrated operation
  • Ruggedized structure for marine and aviation environments
  • Reliable standalone INS performance during GNSS outage
  • Compatible with shipborne, airborne, and unmanned platforms


Application Markets

  • Maritime navigation & ship guidance
  • Survey and offshore engineering vessels
  • Defense and coast guard platforms
  • Aviation guidance and attitude control
  • UAV / USV / UUV inertial guidance
  • Industrial and research institutions


Series Maritime Inertial Navigation System(INS-M)
Type Dubhe-M48
Accelerometer Months Bias Repeatability() 10μg
Months Scale Factor Accuracy() ≤10ppm
Gyro Bias Repeatability() 0.01°/hr
Scale Factor Accuracy() 10ppm
Random walk() 0.003°/hr
Features Angular Rate ≥±400°/sec
Angular Acceleration 100000°/sec2
Acceleration 25g
Speed accuracy(Pure inertia) 0.6kn,RMS
Speed accuracy(GNSS combination) 0.4kn,RMS
Angular Attitude  Any Orientation
Startup time ≤10sec
Input/output 3 RS422 full-duplex serial ports, 1 100M Ethernet port
Alignment time 1hr
Position accuracy Pure inertia 1nm/48h,CEP
INS/DVL Combination 0.3%D,RMS
INS/GNSS Combination better than satellite accuracy
Heading Accuracy Pure inertia 0.04°sec(L),RMS
INS/GNSS combination 0.02°,RMS
Pitch & Roll Accuracy Pure inertia 0.02°,RMS
INS/GNSS combination 0.01°,RMS
Characteristics Power consumption 40W
Dimensions(Lmm×Wmm×Hmm) 232×186×160
Weight 8.2kg
Temperature  -40~60
Shock 15g,Half-sine wave 11ms
Input Voltage DC24V(±25%)
cooling Conduction to mounting plate
Vibration  20~2000Hz,6.06g
MTBF 10000 hours


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