Innalabs Obtained Test Results on its Accelerometer Al-15 at Pennsylvania State University

Jan. 6, 2009 - PRLog -- Innalabs Holding Inc., a leading researcher and manufacturer of inertial systems and sensors for aviation, land and marine applications, have obtained results of independent Al-15 test hold at The Pennsylvania State University.

The objective of this test was to characterize and assess the performance of two single-axis linear accelerometers AL-15 developed by Innalabs. The test results obtained for both AL-15 accelerometers are similar and meet the provided sensor data sheets specification except for the bias value of AL-15-102.

Along with Innalabs Al-15 data was also collected and results provided for another world-famed accelerometer. Two Innalabs accelerometers’ test results were compared to this accelerometer manufactured by another well-known company.

For detailed information on Test Results please contact helen.tselischeva@innalabs.com


About Innalabs® Accelerometers
The Innalabs® Accelerometers are designed as closed-loop pendulous accelerometers with a metallic sensing element (SE), a differential photo-optic displacement sensor (DS) of the SE, and a magneto-electric reverse compensational transducer (RCT).
The Innalabs® Accelerometers make use of a metallic (bronze) sensing element, which provides improved shock and vibration resistance as compared to the quartz based technologies, a feature important to land vehicle applications.  The output of the accelerometers is an analog voltage that is proportional to the acceleration. The zero signal adjustment capability of the differential optical angle transmitter makes it possible to reduce the bias to the minimum. Also, an internal temperature sensor makes it possible to utilize a temperature compensation algorithm to improve the accelerometers performance over a wide temperature range.
Innalabs® Accelerometers have Input range ±2.5, ±30, and ±60 g, Bias < 4 mg, Scale Factor 1.2…1.5 mA/g.

Innalabs Accelerometers Datasheets are available on http://innalabs.com/downloads/


About Innalabs Holding
Innalabs Holding Inc., founded in 2001 as a technology incubator, now is a leading technological company aimed at research, development, sales, support, and manufacturing licensing of advance cost-effective inertial measurement products: Attitude and Heading Reference System (AHRS), Accelerometers, and Gyroscopes. Due to its Research & Development activity, today Innalabs is owner of many patented technologies. Currently Innalabs is developing Inertial Measurement Unit (IMU), Gyrocompass, automotive Event Data Recorder (EDR), Autopilot, etc.
With headquarters in Dulles, VA, Innalabs has R&D Department in CIS and a team of distributors and representatives in Asian region (China, Taiwan).

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Innalabs Holding, Inc. is a leading high-tech company aimed at research, development and manufacturing of inertial navigation systems and sensors like accelerometers, gyroscopes, and Attitude Heading Reference Systems for various applications. Due to its Research & Development activity, today Innalabs is owner of many patented technologies. Currently Innalabs is developing Inertial Measurement Unit (IMU), Gyrocompass, automotive Event Data Recorder (EDR), Autopilot, etc.
With headquarters in Dulles, VA, Innalabs has R&D Department in CIS and a team of distributors and representatives in Asian region (China, Taiwan).