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Low Bias Aviation One Axis Accelerometer For Inclination Measurement

Low Bias Aviation One Axis Accelerometer For Inclination Measurement
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Product: Aviation Accelerometer
Range: +/-70g
Scale Factor Comprehensive Repeatability: ≤15ppm
Nonlinearity Coefficient Comprehensive Repeatability: ≤±10 μg /g2
Working Temp.: -55~+85℃
Consume Current: ≤±20mA
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Low Bias One Axis Accelerometer


Aviation One Axis Accelerometer


accelerometer 1 axis Inclination Measurement

Basic Infomation
Place of Origin: China
Model Number: JB12
Payment & Shipping Terms
Packaging Details: sponge+box
Delivery Time: 10 days for sample
Payment Terms: T/T
Supply Ability: 500/month
Product Description

JB1 navigation accelerometer flexible acceleromete...

aerospace accelerometer low bias aviation accelerometer low cost single axis ship accelerometer



  • Low lag
  • High resolution
  • High accuracy
  • Excellent overload capacity
  • Low cost
  • Broad measurement range

A quartz accelerometer is a force equilibrium sensor,a precise instrument designed according to the principle of ineria.The acceleration input is converted to its fracture's subtle displacement,and then balanced by a feedback force.As a force feedback loop is used,the accelerometer has the features of high precision,high shock resistance,broad measurement range and excellent overload capacity.It is one of the most essential devices in the inertial navigation and guidance system.A quartz accelerometer consists of a gauge excitation circuit and a frequency measurement circuit.The gauge head consists of a dampling plate,a metal pendulum and a force sensitive quartz stick.



  • Drilling
  • Inclination Measurement
  • Aeronautics and Astronautics
  • Instruments and Equipment
  • Oil drilling
  • Flight navigation


Characteristics table


No. Parameters JB11 JB12 JB13
1 Range ±70g ±70g ±70g
2 Threshold 5μg 5μg 5μg
3 Bias K0/K1 ≤±3 mg1 ≤±3 mg ≤±5 mg
4 Scale factor K1 0.8~1.5 mA/g 0.8~1.5 mA/g 0.8~1.5 mA/g
5 Second order nonlinearity coefficient K2 ≤±10μg /g2 ≤±15μg /g2 ≤±20μg /g2
6 0g 4 hours short-term stability ≤10 μg ≤15 μg ≤20 μg
7 1g 4 hours short-term stability ≤10 ppm ≤15 ppm ≤20 ppm
8 Bias comprehensive repeatability σK0 (1σ,1 month) ≤10 μg ≤20 μg ≤30 μg
9 Scale factor comprehensive repeatability σK1/K1 (1σ,1 month) ≤15ppm ≤30 ppm ≤50 ppm
10 Nonlinearity coefficient comprehensive repeatability K2/K1(1σ, 1 month) ≤±10 μg /g2 ≤±20 μg /g2 ≤±30 μg /g2
11 Bias thermal coefficient (full temp. mean) ≤±10 μg /℃ ≤±30 μg /℃ ≤±50 μg /℃
12 Scale factor thermal coefficient (full temp. mean) ≤±10 ppm /℃ ≤±30 ppm /℃ ≤±50 ppm /℃
13 Noise (sampling resistance 840Ω) ≤5mv ≤5mv ≤5mv
14 Natural frequency 400~800 Hz 400~800 Hz 400~800 Hz
15 Bandwidth 800~2500 Hz 800~2500 Hz 800~2500 Hz
16 Random vibration 6g(20-2000Hz) 6g(20-2000Hz) 6g(20-2000Hz)
17 Impact 100g,5ms,1/2sin 100g,5ms,1/2sin 100g,5ms,1/2sin
18 Working temp. -55~+85℃ -55~+85℃ -55~+85℃
19 Store temp. -60~+120℃ -60~+120℃ 60~+120℃
20 Power supply ±12~±15V ±12~±15V ±12~±15V
21 Consume current ≤±20mA ≤±20mA ≤±20mA
22 Thermal sensor Customizable Customizable Customizable
23 Size Ф25.4X30mm Ф25.4X30mm Ф25.4X30mm
24 Weight ≤80g ≤80g ≤80g






Low Bias Aviation One Axis Accelerometer For Inclination Measurement 0



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