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Aviation Navigation TDF71A Airborne Optical Gyro Inertial Navigation

Categories Inertial Navigation System
Brand Name: NAVI OPTICS
Model Number: TDF71A
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: ≤0.01°/hr
Scale Factor Accuracy: ≤20ppm
Random walk: ≤0.005°/√hr
Vibration: 20~2000Hz,6.06g
MTBF: >20000 hours
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Aviation Navigation TDF71A Airborne Optical Gyro Inertial Navigation

Aviation Navigation TDF71A Airborne Optical Gyro Inertial Navigation


1 Introduction

The airborne optical gyro inertial navigation system (INS) employs optical gyroscopes and quartz accelerometers as its core sensing components, utilizing either a strapdown‌ or modulated (dithered) system architecture‌. With high-speed embedded navigation algorithms‌, it delivers real-time positioning and orientation data. This product series integrates satellite-based (GNSS), celestial, barometric altimeter, radio navigation, and visual perception inputs through configurable fusion architectures‌, tailored to mission-specific requirements. Supporting diverse operational modes ranging from standalone inertial navigation‌ to hybrid multi-sensor solutions‌, it provides comprehensive platform navigation parameters including 3D position, velocity, attitude, and angular rates‌.


2 Application Fields

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


3 Performance Characteristics

Supports switching between self-alignment, moving-base alignment, and transfer alignment based on customer needs.

Supports multi-sensor fusion, incorporating satellite, celestial, altimeter, radio, and visual navigation data.

Capable of alignment on ground-based vibrating platforms and in-flight alignment.

Equipped with system fault detection and alarm functions.


4 Main parameters


TypeTDF71A
AccelerometerMonths Bias Repeatability≤20μg
Months Scale Factor Accuracy≤20ppm
GyroBias Repeatability≤0.01°/hr
Scale Factor Accuracy≤20ppm
Random walk≤0.005°/√hr
FeaturesPosition accuracyPure inertia≤2nm/1h
Inertial navigation satellite combinationbetter than satellite accuracy
Velocity accuracyPure inertia≤1.5m/s
Inertial navigation satellite combination≤0.2m/s
Angular Rate≥±400°/sec
Angular Acceleration100000°/sec2
Acceleration>25g
Angular AttitudeAny Orientation
Alignment time≤8min
Input/output3 RS422 full-duplex serial ports, 1 100M Ethernet port
Alignment TimeTime<5min
AHRS Applications PerformanceHeading AccuracyPure inertia≤0.2°sec(L)
Satellite navigation combination≤0.1°sec(L)
Pitch & Roll AccuracyPure inertia≤0.03°
Satellite navigation combination≤0.02°
Power consumption<15W
CharacteristicsDimensions130×130×100
Weight<2.2kg
Temperature-40℃~60℃
Shock15g,Half-sine wave 11ms
Input VoltageDC24V(±25%)
coolingConduction to mounting plate
Vibration20~2000Hz,6.06g
MTBF>20000 hours


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