INT
Buy good quality Aircraft Inertial Navigation System from China INT-A02 GNSS Strapdown Aircraft Inertial Navigation System FOG INS
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Buy good quality Aircraft Inertial Navigation System from China INT-A02 GNSS Strapdown Aircraft Inertial Navigation System FOG INSBuy good quality Aircraft Inertial Navigation System from China INT-A02 GNSS Strapdown Aircraft Inertial Navigation SystemBuy good quality Aircraft Inertial Navigation System from China INT-A02 GNSS Strapdown Aircraft Buy good quality Aircraft Inertial Navigation System from China INT-A02 GNSS INSDetail Information：
Place of Origin
China
Brand Name
Star & Inertia Technology
Model Number
INT-A02
Alignment Time:
≤5min
Position Accuracy/Pure Inertia:
5m/60s(Ref.),150m/300s(Ref.),CEP
Position Accuracy/INS/GNSS Combination:
Better Than GNSS
Speed accuracy/Pure Inertia:
——
Speed accuracy/INS/GNSS Combination:
≤0.2m/s,RMS
Heading Accuracy/Pure Inertia:
≤0.5°secL+0.1°/h,RMS
Heading Accuracy/INS/GNSS Combination:
≤0.3°,RMS
Pitch & Roll Accuracy/Pure Inertia:
≤0.1°,RMS
Pitch & Roll Accuracy/INS/GNSS Combination:
≤0.05°,RMS
Dimensions:
100×100×90mm
Weight:
＜1.35kg
Temperature:
-40℃~60℃
Input Voltage:
DC24V(±25%)
Highlight:
aviation inertial guidance system
,FOG inertial guidance system
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Product Description
Aerospace FOG INS(INT- A02)
Delivering exceptional navigation performance, this optical INS employs FOG/RLG gyros and quartz accelerometers in strapdown configuration. The real-time fusion center combines inertial data with GNSS, celestial and other sources.
Key advantages for UAV applications:
1) Reliable ground/air alignment;
2) Multiple alignment mode selection;
3) Scalable navigation augmentation;
4) Continuous system monitoring.
| Series | Aerospace Inertial Navigation System(INS-A) | ||
| Type | INT-A02 | ||
| Accelerometer | Months Bias Repeatability(1σ) | ≤100μg | |
| Months Scale Factor Accuracy(1σ) | ≤100ppm | ||
| Gyro | Bias Repeatability(1σ) | ≤0.05°/hr | |
| Scale Factor Accuracy(1σ) | ≤100ppm | ||
| Random walk(1σ) | ≤0.02°/√hr | ||
| Features | Position Accuracy | Pure inertia | 5m/60s(Ref.),150m/300s(Ref.),CEP |
| INS/GNSS combination | better than GNSS | ||
| Speed Accuracy | Pure inertia | —— | |
| INS/GNSS combination | ≤0.2m/s,RMS | ||
| Angular Rate | ≥±400°/sec | ||
| Angular Acceleration | 100000°/sec2 | ||
| Acceleration | ＞25g | ||
| Angular Attitude | Any Orientation | ||
| Input/output | 3 RS422 full-duplex serial ports, 1 100M Ethernet port | ||
| Alignment time | ＜5min | ||
| AHRS Applications Performance | Heading Accuracy | Pure inertia | ≤0.5°secL+0.1°/h,RMS |
| INS/GNSS combination | ≤0.3°,RMS | ||
| Pitch & Roll Accuracy | Pure inertia | ≤0.1°,RMS | |
| INS/GNSS combination | ≤0.05°,RMS | ||
| Characteristics | Power consumption | ＜15W | |
| Dimensions | 100×100×90 | ||
| Weight | ＜1.35kg | ||
| 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 | ||
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