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Military INS, Strategic Grade INS, Tactical Grade INS-Inertial navigation system➕Display control
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Military INS, Strategic Grade INS, Tactical Grade INS-Inertial navigation system➕Display control
  • name
  • name

Military INS, Strategic Grade INS, Tactical Grade INS-Inertial navigation system➕Display control

MOQ: a
Standard Packaging: 50cm*40cm*38cm
Delivery Period: 14days
Payment Method: T/T
Supply Capacity: 100/1day
Details Information
Product Description
Detail Information
Place of Origin
wuhan
Brand Name
CSSC
Certification
JKF587412368
Model Number
DP-D-A1
Product Description
 Series Aerospace Inertial Navigation System(INS-A)

Deep pilot Model DP-D-A1
DP-D-A1
Accelerometer Months Bias Repeatability(1σ) ≤30μg
Months Scale Factor Accuracy(1σ) ≤30ppm
Gyro Bias Repeatability(1σ) ≤0.008°/hr
Scale Factor Accuracy(1σ) ≤10ppm
Random walk(1σ) ≤0.003°/√hr
Features Position Accuracy Pure inertia ≤1nm/1h,CEP
INS/GNSS combination better than satellite accuracy
Speed Accuracy Pure inertia ≤1.2m/s,RMS
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 ≤0.05°sec(L),RMS
INS/GNSS combination ≤0.03°,RMS
Pitch & Roll Accuracy Pure inertia ≤0.03°,RMS
INS/GNSS combination ≤0.02°,RMS
Characteristics Power consumption ＜20W
Dimensions(Lmm×Wmm×Hmm) 195×160×108
Weight ＜3.9kg
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


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
Military INS, Strategic Grade INS, Tactical Grade INS-Inertial navigation system➕Display control
  • name
  • name
Military INS, Strategic Grade INS, Tactical Grade INS-Inertial navigation system➕Display control
MOQ: a
Standard Packaging: 50cm*40cm*38cm
Delivery Period: 14days
Payment Method: T/T
Supply Capacity: 100/1day
Detail Information
Product Description
Detail Information
Place of Origin
wuhan
Brand Name
CSSC
Certification
JKF587412368
Model Number
DP-D-A1
Minimum Order Quantity:
a
Packaging Details:
50cm*40cm*38cm
Delivery Time:
14days
Payment Terms:
T/T
Supply Ability:
100/1day
Product Description
 Series Aerospace Inertial Navigation System(INS-A)

Deep pilot Model DP-D-A1
DP-D-A1
Accelerometer Months Bias Repeatability(1σ) ≤30μg
Months Scale Factor Accuracy(1σ) ≤30ppm
Gyro Bias Repeatability(1σ) ≤0.008°/hr
Scale Factor Accuracy(1σ) ≤10ppm
Random walk(1σ) ≤0.003°/√hr
Features Position Accuracy Pure inertia ≤1nm/1h,CEP
INS/GNSS combination better than satellite accuracy
Speed Accuracy Pure inertia ≤1.2m/s,RMS
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 ≤0.05°sec(L),RMS
INS/GNSS combination ≤0.03°,RMS
Pitch & Roll Accuracy Pure inertia ≤0.03°,RMS
INS/GNSS combination ≤0.02°,RMS
Characteristics Power consumption ＜20W
Dimensions(Lmm×Wmm×Hmm) 195×160×108
Weight ＜3.9kg
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


Tags: 

ins gyro,

inertial navigation unit,

navigation gyro

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