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Laser Gyro Inertial Navigation System for Marine & Aviation Guidance – High-Precision INS

Laser Gyro Inertial Navigation System for Marine & Aviation Guidance – High-Precision INS

एमओक्यू: 1 सेट
मूल्य: $1000-$100000
वितरण अवधि: 30 कार्यदिवस
भुगतान विधि: टी/टी
आपूर्ति क्षमता: प्रति वर्ष 100 सेट
विस्तृत जानकारी
उत्पत्ति के प्लेस
चीनी
ब्रांड नाम
Star & Inertia Technology
मॉडल संख्या
दुबे -300
प्रमुखता देना:

Gyro Quartz Laser Inertial Navigation System

,

INS Laser Inertial Navigation System

,

INS gnss aided inertial navigation system

उत्पाद वर्णन

Product Description
The Laser Gyro Inertial Navigation System integrates laser gyroscopes and quartz accelerometers as core sensors. Utilizing a strapdown architecture and advanced real-time navigation software, the system delivers precise navigation and attitude data. It supports multiple operational modes, including inertial/autonomous navigation and inertial-satellite hybrid navigation, providing accurate heading, roll, pitch, speed, and position outputs. The system is suitable for a wide range of maritime and aviation platforms, ensuring good-quality guidance performance for complex operational environments.


Advantages

  • High-precision laser gyro + quartz accelerometer sensors
  • Real-time navigation output with strapdown INS architecture
  • Supports multiple modes: hybrid INS/GNSS and standalone inertial navigation
  • Accurate heading, roll, pitch, speed, and position measurements
  • Ruggedized design for diverse marine and aviation platforms
  • Offered by professional guidance INS guidance system providers and manufacturers


Application

  • Naval and commercial vessels
  • Autonomous Surface/Underwater Vehicles (USV/UUV)
  • Offshore survey and research platforms
  • Aviation attitude and navigation systems
  • Integrated navigation systems for ships and aircraft


Series Maritime Inertial Navigation System(INS-M)
Type Dubhe-M4
Accelerometer Months Bias Repeatability() ≤30μg
Months Scale Factor Accuracy() 30ppm
Gyro Bias Repeatability() 0.003°/hr
Scale Factor Accuracy() 3ppm
Random walk() 0.001°/hr
Features Angular Rate ≥±400°/sec
Angular Acceleration 100000°/sec2
Acceleration 25g
Speed accuracy(Pure inertia) 1.0kn,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 15min
Position accuracy Pure inertia 1nm/4h,CEP
INS/DVL Combination 0.3%D,RMS
INS/GNSS Combination better than satellite accuracy
Heading Accuracy Pure inertia 0.02°sec(L),RMS
INS/GNSS combination 0.01°,RMS
Pitch & Roll Accuracy Pure inertia 0.01°,RMS
INS/GNSS combination 0.01°,RMS
Characteristics Power consumption 30W
Dimensions(Lmm×Wmm×Hmm) 232×186×160
Weight 8kg
Temperature  -40~60
Shock 15g,Half-sine wave 11ms
Input Voltage DC24V(±25%)
cooling Conduction to mounting plate
Vibration 20~2000Hz,6.06g
MTBF 20000 hours



अनुशंसित उत्पाद
उत्पादों
उत्पादों का विवरण
Laser Gyro Inertial Navigation System for Marine & Aviation Guidance – High-Precision INS
एमओक्यू: 1 सेट
मूल्य: $1000-$100000
वितरण अवधि: 30 कार्यदिवस
भुगतान विधि: टी/टी
आपूर्ति क्षमता: प्रति वर्ष 100 सेट
विस्तृत जानकारी
उत्पत्ति के प्लेस
चीनी
ब्रांड नाम
Star & Inertia Technology
मॉडल संख्या
दुबे -300
न्यूनतम आदेश मात्रा:
1 सेट
मूल्य:
$1000-$100000
प्रसव के समय:
30 कार्यदिवस
भुगतान शर्तें:
टी/टी
आपूर्ति की क्षमता:
प्रति वर्ष 100 सेट
प्रमुखता देना

Gyro Quartz Laser Inertial Navigation System

,

INS Laser Inertial Navigation System

,

INS gnss aided inertial navigation system

उत्पाद वर्णन

Product Description
The Laser Gyro Inertial Navigation System integrates laser gyroscopes and quartz accelerometers as core sensors. Utilizing a strapdown architecture and advanced real-time navigation software, the system delivers precise navigation and attitude data. It supports multiple operational modes, including inertial/autonomous navigation and inertial-satellite hybrid navigation, providing accurate heading, roll, pitch, speed, and position outputs. The system is suitable for a wide range of maritime and aviation platforms, ensuring good-quality guidance performance for complex operational environments.


Advantages

  • High-precision laser gyro + quartz accelerometer sensors
  • Real-time navigation output with strapdown INS architecture
  • Supports multiple modes: hybrid INS/GNSS and standalone inertial navigation
  • Accurate heading, roll, pitch, speed, and position measurements
  • Ruggedized design for diverse marine and aviation platforms
  • Offered by professional guidance INS guidance system providers and manufacturers


Application

  • Naval and commercial vessels
  • Autonomous Surface/Underwater Vehicles (USV/UUV)
  • Offshore survey and research platforms
  • Aviation attitude and navigation systems
  • Integrated navigation systems for ships and aircraft


Series Maritime Inertial Navigation System(INS-M)
Type Dubhe-M4
Accelerometer Months Bias Repeatability() ≤30μg
Months Scale Factor Accuracy() 30ppm
Gyro Bias Repeatability() 0.003°/hr
Scale Factor Accuracy() 3ppm
Random walk() 0.001°/hr
Features Angular Rate ≥±400°/sec
Angular Acceleration 100000°/sec2
Acceleration 25g
Speed accuracy(Pure inertia) 1.0kn,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 15min
Position accuracy Pure inertia 1nm/4h,CEP
INS/DVL Combination 0.3%D,RMS
INS/GNSS Combination better than satellite accuracy
Heading Accuracy Pure inertia 0.02°sec(L),RMS
INS/GNSS combination 0.01°,RMS
Pitch & Roll Accuracy Pure inertia 0.01°,RMS
INS/GNSS combination 0.01°,RMS
Characteristics Power consumption 30W
Dimensions(Lmm×Wmm×Hmm) 232×186×160
Weight 8kg
Temperature  -40~60
Shock 15g,Half-sine wave 11ms
Input Voltage DC24V(±25%)
cooling Conduction to mounting plate
Vibration 20~2000Hz,6.06g
MTBF 20000 hours



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