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Aviation Navigation TDL45C Airborne Optical Gyro Inertial Navigation

Categories Inertial Navigation System
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
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Aviation Navigation TDL45C Airborne Optical Gyro Inertial Navigation

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


TypeTDL45C
AccelerometerMonths Bias Repeatability≤20μg
Months Scale Factor Accuracy≤20ppm
GyroBias Repeatability≤0.008°/hr
Scale Factor Accuracy≤20ppm
Random walk≤0.003°/√hr
FeaturesPosition accuracyPure inertia≤1nm/12h
Inertial navigation satellite combinationbetter than satellite accuracy
Velocity accuracyPure inertia≤1.0m/s
Inertial navigation satellite combination≤0.2m/s
Angular Rate≥±400°/sec
Angular Acceleration100000°/sec2
Acceleration>25g
Angular AttitudeAny Orientation
Alignment time≤15min
Input/output3 RS422 full-duplex serial ports, 1 100M Ethernet port
Alignment TimeTime<15min
AHRS Applications PerformanceHeading AccuracyPure inertia≤0.1°sec(L)
Satellite navigation combination≤0.05°sec(L)
Pitch & Roll AccuracyPure inertia≤0.05°
Satellite navigation combination≤0.02°
Power consumption<40W
CharacteristicsDimensions232×186×160
Weight<8.2kg
Temperature-40℃~60℃
Shock15g,Half-sine wave 11ms
Input VoltageDC24V(±25%)
CoolingConduction to mounting plate
Vibration20~2000Hz,6.06g
MTBF>15000 hours


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