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TDF61A Airborne Optical Gyro-Inertial Navigation
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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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