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TDF61A Airborne Optical Gyro-Inertial Navigation

The vehicle-mounted optical gyro positioning and orientation device uses laser or fiber optic gyros and quartz accelerometers as core sensors. It employs a strapdown inertial navigation system architecture and runs advanced navigation software to provide real-time navigation information. The product series features multiple operating modes, including zero-velocity update (ZUPT), inertial/satellite-based integrated navigation, and inertial/odometer integrated navigation. It provides users with complete navigation parameters for the vehicle, meeting the needs of various vehicle-mounted platforms.

Keyword:

Introduction

Accessories

Recommendations

 

Model

 

TDF61A

 

 

Accelerometer

Months Bias Repeatability

≤50μg

Months Scale Factor Accuracy

≤50ppm

 

 

 

Gyro

Bias Repeatability

≤0.03°/hr,1σ

Scale Factor Accuracy

≤50ppm

Random walk

≤0.01°/√hr

 

 

 

 

 

 

 

 

Features

Angular Rate

≥±400°/sec

Angular Acceleration

100000°/sec2

Acceleration

>40g

 Angular Attitude

Any Orientation

Alignment time

≤5min

Input/output

3 RS422 full-duplex serial ports, 1 100M Ethernet port

 

 

 

 

 

 

 

Position accuracy

North finding/orientation accuracy

--

Inertial navigation/odometer combination

≤1%D

North finding/orientation accuracy

≤5.0mil

Bearing keeping accuracy/2h

≤6.0mil

Combined navigation position accuracy

≤3.0mil

 

 

AHRS Applications Performance

Heading Accuracy

≤3.0mil

Pitch & Roll Accuracy

≤1.0mil

 

 

 

 

 

 

 

 

 

 

 

 

 

Characteristics

Power consumption

<15W

Dimensions

110×110×100

Weight

<1.7kg

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

 

Application field

Suitable for geodetic survey vehicles, tanks, self-propelled artillery, infantry fighting vehicles, unmanned vehicles, high-speed trains, agricultural machinery vehicles, etc.

 

 

Performance characteristics

  • Capable of alignment and initialization in static or dynamic (in-motion) states.
  • Features autonomous navigation, zero-velocity update (ZUPT), and integrated navigation with odometer and/or satellite-based systems.
  • Suitable for use in high-latitude (±65°), extremely cold, and high-altitude regions.
  • High reliability.

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