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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

Name: Jammingresistant Fully Autonomous High Precision Inertial Navigation System INS for Aerospace Applications
Brand: CSSC
Price: 1200000 USD

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

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

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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

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

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