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Jamming-resistant Fully Autonomous High Precision Inertial Navigation System (INS) for Aerospace Applications
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Jamming-resistant Fully Autonomous High Precision Inertial Navigation System (INS) for Aerospace Applications

MOQ: 1
Price: 1200000
Standard Packaging: 40CM*40CM*50CM
Delivery Period: 4weeks
Payment Method: T/T
Supply Capacity: 10PS/4weeks
Details Information
Product Description
Detail Information
Place of Origin
hubei
Brand Name
CSSC
Certification
AKJ5852596575
Model Number
DP-M-A03000
Accelerometer Bias Repeatability:
≤50μg
Gyro Bias Repeatability:
≤0.02°/hr
Angular Rate:
≥±400°/sec
Power Consumption:
＜15W
Dimensions:
110*110*100mm
Weight:
＜1.7kg
Product 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
Tags: 

ins gyro,  

inertial navigation unit,  

navigation gyro

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Products
PRODUCTS DETAILS
Products

Laser Inertial Navigation System

Fiber Optic Inertial Navigation System

Aircraft Inertial Navigation System

Marine Inertial Navigation System

Automotive Inertial Navigation System

AHRS System

IMU Inertial Measurement Unit

Fiber Optic Gyroscope

Ring Laser Gyroscope

Doppler Velocity Log

MEMS Inertial Navigation System
  • name
  • name
  • name
  • name
  • name
Jamming-resistant Fully Autonomous High Precision Inertial Navigation System (INS) for Aerospace Applications
MOQ: 1
Price: 1200000
Standard Packaging: 40CM*40CM*50CM
Delivery Period: 4weeks
Payment Method: T/T
Supply Capacity: 10PS/4weeks
Detail Information
Product Description
Detail Information
Place of Origin
hubei
Brand Name
CSSC
Certification
AKJ5852596575
Model Number
DP-M-A03000
Accelerometer Bias Repeatability:
≤50μg
Gyro Bias Repeatability:
≤0.02°/hr
Angular Rate:
≥±400°/sec
Power Consumption:
＜15W
Dimensions:
110*110*100mm
Weight:
＜1.7kg
Minimum Order Quantity:
1
Price:
1200000
Packaging Details:
40CM*40CM*50CM
Delivery Time:
4weeks
Payment Terms:
T/T
Supply Ability:
10PS/4weeks
Product 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
Tags: 

ins gyro,

inertial navigation unit,

navigation gyro

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