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AHRS Dynamic Attitude Resolution and Application of AHRS Measurement Unit in UAV Flight Control Systems
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AHRS Dynamic Attitude Resolution and Application of AHRS Measurement Unit in UAV Flight Control Systems
  • name
  • name
  • name
  • name

AHRS Dynamic Attitude Resolution and Application of AHRS Measurement Unit in UAV Flight Control Systems

MOQ: 1
Standard Packaging: 30cm*30cm*28cm
Delivery Period: 14days
Payment Method: T/T
Supply Capacity: 50/1day
Details Information
Product Description
Detail Information
Place of Origin
WUHAN
Brand Name
CSSC
Certification
kjd527896520
Model Number
DP-M-H01AA
Outputformat:
Digital (UART, SPI, CAN)
Vibration:
20~2000Hz,6.06g
Angular Acceleration:
100000°/sec2
Alignment Time:
＜10min
Type:
Attitude And Heading Reference System
Mtbf:
＞20000 Hours
Shock:
15g，Half-sine Wave 11ms
Productname:
AHRS System
Power Consumption:
＜10W
Sensortype:
MEMS Gyroscopes And Accelerometers
Angular Rate:
≥±400°/sec
Product Description
 Series Attitude and Heading Reference Systems(AHRS)
Deep pilot Model DP-M-H01AA
Accelerometer Months Bias Repeatability(1σ) ≤500μg
Months Scale Factor Accuracy(1σ) ≤500ppm
Gyro Bias Repeatability(1σ) ≤0.1°/hr
Scale Factor Accuracy(1σ) ≤300ppm
Random walk(1σ) ≤0.03°/√hr
Features Angular Rate ≥±400°/sec
Angular Acceleration 100000°/sec2
Acceleration ＞40g
Angular Attitude  Any Orientation
Startup time 10 sec
Input/output 3 RS422 full-duplex serial ports, 1 100M Ethernet port
Alignment time ＜10min
AHRS Applications Performance Heading Accuracy Pure inertia ≤1.0°secL+0.2°/h,RMS
INS/Single-antenna  GNSS combination ≤0.5°,RMS
INS/Dual-antenna GNSS combination ≤0.1°,RMS
Pitch & Roll Accuracy Pure inertia ≤0.15°,RMS
INS/GNSS combination ≤0.1°,RMS
Characteristics Power consumption ＜10W
Dimensions(Lmm×Wmm×Hmm) 70×70×53
Weight ＜500g
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: 

attitude heading reference system,  

system ahrs,  

ahrs mems

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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
AHRS Dynamic Attitude Resolution and Application of AHRS Measurement Unit in UAV Flight Control Systems
  • name
  • name
  • name
  • name
AHRS Dynamic Attitude Resolution and Application of AHRS Measurement Unit in UAV Flight Control Systems
MOQ: 1
Standard Packaging: 30cm*30cm*28cm
Delivery Period: 14days
Payment Method: T/T
Supply Capacity: 50/1day
Detail Information
Product Description
Detail Information
Place of Origin
WUHAN
Brand Name
CSSC
Certification
kjd527896520
Model Number
DP-M-H01AA
Outputformat:
Digital (UART, SPI, CAN)
Vibration:
20~2000Hz,6.06g
Angular Acceleration:
100000°/sec2
Alignment Time:
＜10min
Type:
Attitude And Heading Reference System
Mtbf:
＞20000 Hours
Shock:
15g，Half-sine Wave 11ms
Productname:
AHRS System
Power Consumption:
＜10W
Sensortype:
MEMS Gyroscopes And Accelerometers
Angular Rate:
≥±400°/sec
Minimum Order Quantity:
1
Packaging Details:
30cm*30cm*28cm
Delivery Time:
14days
Payment Terms:
T/T
Supply Ability:
50/1day
Product Description
 Series Attitude and Heading Reference Systems(AHRS)
Deep pilot Model DP-M-H01AA
Accelerometer Months Bias Repeatability(1σ) ≤500μg
Months Scale Factor Accuracy(1σ) ≤500ppm
Gyro Bias Repeatability(1σ) ≤0.1°/hr
Scale Factor Accuracy(1σ) ≤300ppm
Random walk(1σ) ≤0.03°/√hr
Features Angular Rate ≥±400°/sec
Angular Acceleration 100000°/sec2
Acceleration ＞40g
Angular Attitude  Any Orientation
Startup time 10 sec
Input/output 3 RS422 full-duplex serial ports, 1 100M Ethernet port
Alignment time ＜10min
AHRS Applications Performance Heading Accuracy Pure inertia ≤1.0°secL+0.2°/h,RMS
INS/Single-antenna  GNSS combination ≤0.5°,RMS
INS/Dual-antenna GNSS combination ≤0.1°,RMS
Pitch & Roll Accuracy Pure inertia ≤0.15°,RMS
INS/GNSS combination ≤0.1°,RMS
Characteristics Power consumption ＜10W
Dimensions(Lmm×Wmm×Hmm) 70×70×53
Weight ＜500g
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: 

attitude heading reference system,

system ahrs,

ahrs mems

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