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Jamming-resistant Fully Autonomous High Precision Inertial Navigation System (INS) for Aerospace Applications
Jamming-resistant Fully Autonomous High Precision Inertial Navigation System (INS) for Aerospace Applications
Jamming-resistant Fully Autonomous High Precision Inertial Navigation System (INS) for Aerospace Applications
Jamming-resistant Fully Autonomous High Precision Inertial Navigation System (INS) for Aerospace Applications
Jamming-resistant Fully Autonomous High Precision Inertial Navigation System (INS) for Aerospace Applications
Jamming-resistant Fully Autonomous High Precision Inertial Navigation System (INS) for Aerospace Applications
Jamming-resistant Fully Autonomous High Precision Inertial Navigation System (INS) for Aerospace Applications
Jamming-resistant Fully Autonomous High Precision Inertial Navigation System (INS) for Aerospace Applications
Specifications
Model Number :
DP-M-A03000
Gyro Bias Repeatability :
≤0.02°/hr
Payment Terms :
T/T
Supply Ability :
10PS/4weeks
Brand Name :
CSSC
Accelerometer Bias Repeatability :
≤50μg
Packaging Details :
40CM*40CM*50CM
MOQ :
1
Delivery Time :
4weeks
Dimensions :
110*110*100mm
Price :
1200000
Weight :
＜1.7kg
Certification :
AKJ5852596575
Angular Rate :
≥±400°/sec
Place of Origin :
hubei
Power consumption :
＜15W
Description
Jamming-resistant Inertial Navigation Systems
Fully autonomous aerospace inertial navigation systems designed for precision and reliability in demanding environments.
Product Series
Aerospace Inertial Navigation System (INS-A)
Technical Specifications
Parameter Specification
Deep Pilot Model DP-M-A03
Accelerometer - Months Bias Repeatability (1σ) ≤50μg
Accelerometer - Months Scale Factor Accuracy (1σ) ≤50ppm
Gyro - Bias Repeatability (1σ) ≤0.02°/hr
Gyro - Scale Factor Accuracy (1σ) ≤50ppm
Gyro - Random walk (1σ) ≤0.01°/√hr
Performance Features
Feature Performance
Position Accuracy - Pure inertia ≤4nm/1h, CEP
Position Accuracy - INS/GNSS combination Better than satellite accuracy
Speed Accuracy - Pure inertia ≤3.0m/s, RMS
Speed Accuracy - INS/GNSS combination ≤0.2m/s, RMS
Angular Rate ≥±400°/sec
Angular Acceleration 100000°/sec²
Acceleration ＞25g
Angular Attitude Any Orientation
Interface & Alignment
Parameter Specification
Input/Output 3 RS422 full-duplex serial ports, 1 100M Ethernet port
Alignment Time ＜5min
AHRS Applications Performance
Parameter Performance
Heading Accuracy - Pure inertia ≤0.2°sec(L), RMS
Heading Accuracy - INS/GNSS combination ≤0.1°, RMS
Pitch & Roll Accuracy - Pure inertia ≤0.05°, RMS
Pitch & Roll Accuracy - INS/GNSS combination ≤0.03°, RMS
Physical Characteristics
Characteristic Specification
Power Consumption ＜15W
Dimensions (L×W×H) 110×110×100 mm
Weight ＜1.7kg
Operating Temperature -40℃ to +60℃
Shock Resistance 15g, Half-sine wave 11ms
Input Voltage DC24V (±25%)
Cooling Method Conduction to mounting plate
Vibration Resistance 20-2000Hz, 6.06g
MTBF ＞22000 hours
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Jamming-resistant Fully Autonomous High Precision Inertial Navigation System (INS) for Aerospace Applications

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Product Detail
Model Number :
DP-M-A03000
Gyro Bias Repeatability :
≤0.02°/hr
Payment Terms :
T/T
Supply Ability :
10PS/4weeks
Brand Name :
CSSC
Accelerometer Bias Repeatability :
≤50μg
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Jamming-resistant Fully Autonomous High Precision Inertial Navigation System (INS) for Aerospace Applications
Jamming-resistant Fully Autonomous High Precision Inertial Navigation System (INS) for Aerospace Applications
Jamming-resistant Fully Autonomous High Precision Inertial Navigation System (INS) for Aerospace Applications
Jamming-resistant Fully Autonomous High Precision Inertial Navigation System (INS) for Aerospace Applications

CSSC Star&Inertia Technology co.,ltd.

Verified Supplier
2 Years
hubei, wuhan
Since 2013
Business Type :
Manufacturer
Main Products :
Laser Inertial Navigation System, Fiber Optic Inertial Navigation System, Aircraft Inertial Navigation System
Total Annual :
5000000-10000000
Employee Number :
300~500
Certification Level :
Verified Supplier
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