Jurnal Teknologi Dirgantara
Vol.10 No.2 Desember 2012

METODE KALIBRASI SENSOR RATE-GYROSCOPE UNTUK IMU ROKET [CALIBRATION METHOD OF RATE-GYROSCOPE SENSOR FOR IMU ROCKET]

- Wahyudi (Bidang Telemetri fan Muatan Roket, LAPAN)
Adhi Susanto (Fakultas Teknik, Universitas Gadjah Mada)
Wahyu Widada Wahyu Widada (Bidang Telemetri fan Muatan Roket, LAPAN)
Sasongko Pramono Hadi (Fakultas Teknik, Universitas Gadjah Mada)



Article Info

Publish Date
15 Mar 2013

Abstract

Rate-gyroscope sensor is used in the IMU to measure the rotation angle in three axes. The output of rate-gyroscope sensor is a voltage which is the angular rate, so to obtain the angle used once an integral process. The integral result of rate-gyroscope sensor depend on sampling time or the cycle time of program to get the datum, so the integral calculation depends on the processor speed of microcontroller (computer). Using of the different sampling time will affect the integral result or in other words we can say that for the same program, if we apply it to a different microcontroller, we will obtain the different calculation. This paper presents the calibration method for determining the calibration factor on the rate-gyroscope sensor, so we will get the actual angle value. The rate-gyroscope sensors on different axes have different characteristics, so each sensor needs to be calibrated. In the experiment results, the calibration factors in three axes are different in both for the clockwise rotation and counterclockwise rotation. Key words: Calibration, Rate-gyroscope, IMU

Copyrights © 2012






Journal Info

Abbrev

jurnal_tekgan

Publisher

Subject

Aerospace Engineering Chemical Engineering, Chemistry & Bioengineering Computer Science & IT Mechanical Engineering Physics

Description

Jurnal Teknologi Dirgantara (Journal of Aerospace Technology) is an Indonesian accredited scientific publication that covers topics of Rocket, satellite, and aeronautics technology, as well as a spin-off from aerospace technology, such as aerodynamics, astronautics, aerospace structure, power and ...