| MOQ: | 1 |
| Standard Packaging: | 50cm*40cm*38cm |
| Delivery Period: | 30days |
| Payment Method: | T/T |
| Supply Capacity: | 10/1day |
| Series | Aerospace Inertial Navigation System(INS-A) | Aerospace Inertial Navigation System(INS-A) | |||
| Deep pilot Model | DP-M-A01 | DP-D-A20 | |||
| Accelerometer | Months Bias Repeatability(1σ) | ≤500μg | ≤10μg | ||
| Months Scale Factor Accuracy(1σ) | ≤500ppm | ≤10ppm | |||
| Gyro | Bias Repeatability(1σ) | ≤0.1°/hr | ≤0.008°/hr | ||
| Scale Factor Accuracy(1σ) | ≤300ppm | ≤10ppm | |||
| Random walk(1σ) | ≤0.03°/√hr | ≤0.003°/√hr | |||
| Features | Position Accuracy | Pure inertia | 20m/60s(Ref.),500m/300s(Ref.),CEP | ≤1nm/20h,CEP | |
| INS/GNSS combination | better than satellite accuracy | better than satellite accuracy | |||
| Speed Accuracy | Pure inertia | —— | ≤1.0 m/s,RMS | ||
| INS/GNSS combination | ≤0.2m/s,RMS | ≤0.2m/s,RMS | |||
| Angular Rate | ≥±400°/sec | ≥±400°/sec | |||
| Angular Acceleration | 100000°/sec2 | 100000°/sec2 | |||
| Acceleration | >40g | >25g | |||
| Angular Attitude | Any Orientation | Any Orientation | |||
| Input/output | 2 RS422 serial ports | 3 RS422 full-duplex serial ports, 1 100M Ethernet port | |||
| Alignment time | <5min | <30min | |||
| AHRS Applications Performance | Heading Accuracy | Pure inertia | ≤1.0°secL+0.2°/h,RMS | ≤0.02°sec(L),RMS | |
| INS/GNSS combination | ≤0.5°,RMS | ≤0.01°,RMS | |||
| Pitch & Roll Accuracy | Pure inertia | ≤0.2°,RMS | ≤0.02°,RMS | ||
| INS/GNSS combination | ≤0.1°,RMS | ≤0.01°,RMS | |||
| Characteristics | Power consumption | <10W | <40W | ||
| Dimensions(Lmm×Wmm×Hmm) | 70×70×53 | 232×186×160 | |||
| Weight | <500g | <8.2kg | |||
| Temperature | -40℃~60℃ | -40℃~60℃ | |||
| Shock | 15g,Half-sine wave 11ms | 15g,Half-sine wave 11ms | |||
| Input Voltage | DC24V(±25%) | DC24V(±25%) | |||
| cooling | Conduction to mounting plate | Conduction to mounting plate | |||
| Vibration | 20~2000Hz,6.06g | 20~2000Hz,6.06g | |||
| MTBF | >20000 hours | >10000 hours | |||
| MOQ: | 1 |
| Standard Packaging: | 50cm*40cm*38cm |
| Delivery Period: | 30days |
| Payment Method: | T/T |
| Supply Capacity: | 10/1day |
| Series | Aerospace Inertial Navigation System(INS-A) | Aerospace Inertial Navigation System(INS-A) | |||
| Deep pilot Model | DP-M-A01 | DP-D-A20 | |||
| Accelerometer | Months Bias Repeatability(1σ) | ≤500μg | ≤10μg | ||
| Months Scale Factor Accuracy(1σ) | ≤500ppm | ≤10ppm | |||
| Gyro | Bias Repeatability(1σ) | ≤0.1°/hr | ≤0.008°/hr | ||
| Scale Factor Accuracy(1σ) | ≤300ppm | ≤10ppm | |||
| Random walk(1σ) | ≤0.03°/√hr | ≤0.003°/√hr | |||
| Features | Position Accuracy | Pure inertia | 20m/60s(Ref.),500m/300s(Ref.),CEP | ≤1nm/20h,CEP | |
| INS/GNSS combination | better than satellite accuracy | better than satellite accuracy | |||
| Speed Accuracy | Pure inertia | —— | ≤1.0 m/s,RMS | ||
| INS/GNSS combination | ≤0.2m/s,RMS | ≤0.2m/s,RMS | |||
| Angular Rate | ≥±400°/sec | ≥±400°/sec | |||
| Angular Acceleration | 100000°/sec2 | 100000°/sec2 | |||
| Acceleration | >40g | >25g | |||
| Angular Attitude | Any Orientation | Any Orientation | |||
| Input/output | 2 RS422 serial ports | 3 RS422 full-duplex serial ports, 1 100M Ethernet port | |||
| Alignment time | <5min | <30min | |||
| AHRS Applications Performance | Heading Accuracy | Pure inertia | ≤1.0°secL+0.2°/h,RMS | ≤0.02°sec(L),RMS | |
| INS/GNSS combination | ≤0.5°,RMS | ≤0.01°,RMS | |||
| Pitch & Roll Accuracy | Pure inertia | ≤0.2°,RMS | ≤0.02°,RMS | ||
| INS/GNSS combination | ≤0.1°,RMS | ≤0.01°,RMS | |||
| Characteristics | Power consumption | <10W | <40W | ||
| Dimensions(Lmm×Wmm×Hmm) | 70×70×53 | 232×186×160 | |||
| Weight | <500g | <8.2kg | |||
| Temperature | -40℃~60℃ | -40℃~60℃ | |||
| Shock | 15g,Half-sine wave 11ms | 15g,Half-sine wave 11ms | |||
| Input Voltage | DC24V(±25%) | DC24V(±25%) | |||
| cooling | Conduction to mounting plate | Conduction to mounting plate | |||
| Vibration | 20~2000Hz,6.06g | 20~2000Hz,6.06g | |||
| MTBF | >20000 hours | >10000 hours | |||