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Aviation Navigation TDL45C Airborne Optical Gyro Inertial Navigation
Aviation Navigation TDL45C Airborne Optical Gyro Inertial Navigation
Specifications
Brand Name :
NAVI OPTICS
Model Number :
TDL45C
Certification :
CCS
Place of Origin :
China
MOQ :
one set
Payment Terms :
L/C,T/T
Supply Ability :
10 sets per month
Delivery Time :
5-8 work days
Packaging Details :
Carton box
Months Bias Repeatability :
≤20μg
Months Scale Factor Accuracy :
≤20ppm
Bias Repeatability :
≤0.008°/hr
Scale Factor Accuracy :
≤20ppm
Random walk :
≤0.003°/√hr
Vibration :
20~2000Hz,6.06g
MTBF :
＞15000 hours
Description

Aviation Navigation TDL45C Airborne Optical Gyro Inertial Navigation


1 Introduction

The airborne optical gyro inertial navigation system (INS) utilizes optical gyros and quartz accelerometers as its core sensors, employing either a strapdown or dithered (modulated) inertial navigation system architecture. It runs advanced navigation software internally at high speed to provide real-time navigation information. This series of products can integrate satellite, celestial, altimeter, radio, and visual navigation information, based on user requirements. It supports multiple operating modes, including purely inertial and multi-sensor fusion, providing users with complete navigation parameters for their platforms.


2 Application Fields

Suitable for fixed-wing UAVs, rotary-wing UAVs, and specialized airborne vehicles.


3 Performance Characteristics

Enables alignment capabilities for both stationary ground platforms with vibration interference and in-flight navigation systems.
Features adaptive alignment mode switching (self-alignment, moving-base alignment, transfer alignment) to meet mission-specific requirements.
Integrates multi-source navigation data through advanced sensor fusion technology, including satellite, celestial, barometric, radio aids, and visual odometry inputs.
Incorporates built-in health monitoring with real-time fault diagnostics and alert mechanisms.


4 Main parameters


Type TDL45C
Accelerometer Months Bias Repeatability ≤20μg
Months Scale Factor Accuracy ≤20ppm
Gyro Bias Repeatability ≤0.008°/hr
Scale Factor Accuracy ≤20ppm
Random walk ≤0.003°/√hr
Features Position accuracy Pure inertia ≤1nm/12h
Inertial navigation satellite combination better than satellite accuracy
Velocity accuracy Pure inertia ≤1.0m/s
Inertial navigation satellite combination ≤0.2m/s
Angular Rate ≥±400°/sec
Angular Acceleration 100000°/sec2
Acceleration ＞25g
Angular Attitude Any Orientation
Alignment time ≤15min
Input/output 3 RS422 full-duplex serial ports, 1 100M Ethernet port
Alignment Time Time ＜15min
AHRS Applications Performance Heading Accuracy Pure inertia ≤0.1°sec(L)
Satellite navigation combination ≤0.05°sec(L)
Pitch & Roll Accuracy Pure inertia ≤0.05°
Satellite navigation combination ≤0.02°
Power consumption ＜40W
Characteristics Dimensions 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 ＞15000 hours


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Aviation Navigation TDL45C Airborne Optical Gyro Inertial Navigation

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Product Detail
Brand Name :
NAVI OPTICS
Model Number :
TDL45C
Certification :
CCS
Place of Origin :
China
MOQ :
one set
Payment Terms :
L/C,T/T
Contact Supplier
Aviation Navigation TDL45C Airborne Optical Gyro Inertial Navigation

QINGDAO THUNDSEA MARINE TECHNOLOGY CO.,LTD

Verified Supplier
6 Years
Since 2014
Business Type :
Manufacturer, Distributor/Wholesaler, Agent, Importer, Exporter
Main Products :
Inertial Navigation System, Laser Inertial Navigation System, Fiber Optic Gyrocompass
Total Annual :
4,800,000-5,200,000
Employee Number :
100~120
Certification Level :
Verified Supplier
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