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Products — Quartz Gyros

INNALABS designs, produces and manufactures: Quartz Gyros

Quartz Gyroscopes


INNALABS' INN-105/106/107 Quartz Gyroscopes are single-, dual-, and three-axis angular rate analog gyroscope sensor which utilizes vibrating quartz technology where the Coriolis Effect is used to measure angular rotation rate. The INNALABS' INN-108 Quartz gyroscope is compact, highly reliable, solid-state single-axis angular rotation sensors based on monolithic quartz sensing element, and features internal power regulation, and designed for use by original equipment manufacturers (OEM.

Applications: Antennas and platforms stabilization through a gyroscope, robotics and various vehicles control and stabilization, low-cost inertial systems, such as Inertial Navigation Systems (INS) or Inertial Measurement Units (IMU) or any others that uses a gyroscope sensor, different measurement purposes in precision farming, factory automation, medical, and orthopedic applications.

  

Bricett Quartz Gyros

Technical Specifications

Parameters Units Values
 Number of axis   1 - axis gyroscopes 2 - axis gyroscopes 3 - axis gyroscopes
 Datasheets  

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 Picture   Bricett Quartz Gyros Bricett Quartz Gyros Bricett Quartz Gyros Bricett Quartz Gyros
 Type   INN-108 INN-105 INN-106 INN-107
 Version   - 1.1 1.2 2.1 2.2 3.1 3.2 1.1 1.2 2.1 2.2 3.1 3.2 1.1 1.2 2.1 2.2 3.1 3.2
 Measurement Range deg/s ±50, ±100, ±200,±500 ±50
 ±200 ±50 ±500 ±100 ±3000 ±50 ±200 ±50 ±500 ±100 ±3000 ±50 ±200 ±50 ±500 ±100 ±3000
 Bias stability at const.
 temp., 10 sec
 averaging time		 deg/s ≤0.05 ≤0.02 ≤0.4 ≤0.04 ≤0.06 ≤0.06 ≤0.3 ≤0.02 ≤0.4 ≤0.04 ≤0.06 ≤0.06 ≤0.3 ≤0.02 ≤0.4 ≤0.04 ≤0.06 ≤0.06 ≤0.3
 Sensitivity deg/s - ≤0.01 ≤0.02 ≤0.015 ≤0.1 ≤0.02 ≤0.2 ≤0.01 ≤0.02 ≤0.015 ≤0.1 ≤0.02 ≤0.2 ≤0.01 ≤0.02 ≤0.015 ≤0.1 ≤0.02 ≤0.2
 Scale Factor
 nonlinearity		 %FS ≤0.05 ≤0.05 ≤0.08 ≤0.2 ≤0.05 ≤0.08 ≤0.2 ≤0.05 ≤0.08 ≤0.2
 Dimensions (L x W x H) mm 69x26x26 15 x 30 x 50
 30 x 31 x 54
 30 x 40 x 50
 Weight grams ≤50 60 100 120
 Input Current mA - 10 or 20 20 or 40 30 or 60
 Full Scale Output V 0…5 or ±5 0 – 5 or ±5
 Bias Calibration (at
 normal temperature)		 V - 2.5±0.05 or 0±0.05
 G Sensitivity deg/s/g ≤0.06 ≤0.06
 Angle Random Walk deg/√h ≤0.02 1 … 1.5
 Start up time sec ≤1 1
 Bandwidth Hz >50 60
 Operating temperature ⁰C -40…+85 -40 … +70
 Storage temperature ⁰C -55…+100 -55 … +85
 Vibration g, RMS 5g, 20…2000Hz 2 g, 20 Hz … 2 kHz random
 Shock g 200 500 g, 5 ms
 Data interface   - Analog
 Input Voltages V +8…+18 or ±8…±18 +8 … +12 or ±8 … ±12


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INNALABS
Phone: +353 1 888 1008.
contact.sales@innalabs.com

INNALABS develops high-performance inertial navigation systems that focus on critical stabilization, control, navigation and guidance applications. The state-of-the-art products, such as an accelerometer and gyroscope, are used in the aerospace and commercial aircraft markets across the world. Our products soar above the competition in precision and cutting-edge technology thanks to our dedicated Research and Development Department.