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Aviation Navigation TDF61A Airborne Optical Gyro Inertial Navigation

Categories Inertial Navigation System
Brand Name: NAVI OPTICS
Model Number: TDF61A
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: ≤50μg
Months Scale Factor Accuracy: ≤500ppm
Bias Repeatability: ≤0.3°/hr
Scale Factor Accuracy: ≤500ppm
Random walk: ≤0.01°/√hr
Vibration: 20~2000Hz,6.06g
MTBF: >20000 hours
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Aviation Navigation TDF61A Airborne Optical Gyro Inertial Navigation

Aviation Navigation TDF61A Airborne Optical Gyro Inertial Navigation


1 Introduction

The airborne optical gyro inertial navigation system (INS) employs optical gyros and quartz accelerometers as its core sensing components, operating under either a strapdown or dither-modulated inertial navigation architecture‌. High-speed embedded navigation software processes sensor data in real time to deliver continuous positioning and orientation outputs‌. This product series integrates multi-source navigation inputs including satellite signals (GNSS), celestial observations, barometric altimetry, radio navigation aids, and visual odometry based on mission-specific configurations‌. It offers operational flexibility through selectable modes ranging from standalone inertial navigation to adaptive multi-sensor fusion, delivering comprehensive platform states (position, velocity, attitude) across dynamic environments‌.


2 Application Fields

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


3 Performance Characteristics

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

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.

Equipped with system fault detection and alarm functions.


4 Main parameters


TypeTDF61A
AccelerometerMonths Bias Repeatability≤50μg
Months Scale Factor Accuracy≤500ppm
GyroBias Repeatability≤0.3°/hr
Scale Factor Accuracy≤500ppm
Random walk≤0.01°/√hr
FeaturesPosition accuracyPure inertia≤4nm/1h
Inertial navigation satellite combinationbetter than satellite accuracy
Velocity accuracyPure inertia≤3.0m/s
Inertial navigation satellite combination≤0.2m/s
Angular Rate≥±400°/sec
Angular Acceleration100000°/sec2
Acceleration>25g
Angular AttitudeAny Orientation
Alignment time≤5min
Input/output3 RS422 full-duplex serial ports, 1 100M Ethernet port
Alignment TimeTime<5min
AHRS Applications PerformanceHeading AccuracyPure inertia≤0.4°sec(L)
Satellite navigation combination≤0.2°sec(L)
Pitch & Roll AccuracyPure inertia≤0.08°
Satellite navigation combination≤0.03°
CharacteristicsPower consumption<15W
Dimensions110×110×100
Weight<1.7kg
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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