Measurement and analysis of certain flight parameters based on MEMS sensors
Gyroscopes established one of the fundamental references for attitude and heading in aerospace applications. The information about angular velocities gives input not only for autopilot, but also damping devices, such as yaw or pitch dampers for example. The MEMS (micro-electro-mechanical system) gyr...
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| Veröffentlicht in: | Journal of sensors and sensor systems 2017-05, Vol.6 (1), p.211-222 |
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| creator | Bakunowicz, Jerzy Rzucid?o, Pawel |
| description | Gyroscopes established one of the fundamental references for attitude and heading in aerospace applications. The information about angular velocities gives input not only for autopilot, but also damping devices, such as yaw or pitch dampers for example. The MEMS (micro-electro-mechanical system) gyroscopes are much less reliable than their laser or fibre-optic cousins. Nevertheless, the availability and low price of MEMS components make this a growing area of application in avionics for general aviation aeroplanes. This paper presents certain results of flight data analysis registered during the flight testing campaign of the new experimental low-power single-engine turbo-propeller utility aeroplane I-31T. The research was focused on identification of oscillation modes, distinctive for the new aeroplane, such as engine precession or shimmy. The data came from a three-axis MEMS gyroscope and accelerometer recorder, placed near to the centre of gravity. Wavelet transform, which was used for analysis, gave better precision in time domain than Fourier transform, especially for signals of low frequency. |
| doi_str_mv | 10.5194/jsss-6-211-2017 |
| format | Article |
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The information about angular velocities gives input not only for autopilot, but also damping devices, such as yaw or pitch dampers for example. The MEMS (micro-electro-mechanical system) gyroscopes are much less reliable than their laser or fibre-optic cousins. Nevertheless, the availability and low price of MEMS components make this a growing area of application in avionics for general aviation aeroplanes. This paper presents certain results of flight data analysis registered during the flight testing campaign of the new experimental low-power single-engine turbo-propeller utility aeroplane I-31T. The research was focused on identification of oscillation modes, distinctive for the new aeroplane, such as engine precession or shimmy. The data came from a three-axis MEMS gyroscope and accelerometer recorder, placed near to the centre of gravity. 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| subjects | Accelerometers Aeronautics Aircraft Aircraft components Analysis Angular velocity Automatic pilots Aviation Avionics Center of gravity Dampers Damping Data analysis Devices Fiber optics Flight data recorders Flight tests Fourier analysis Fourier transforms General aviation Gyroscopes Lasers Load Measurement Measurement techniques Mechanical systems Microelectromechanical systems Optical fibers Oscillation modes Pitch (inclination) Precession Sensors Testing Three axis Wavelet analysis Wavelet transforms Yaw |
| title | Measurement and analysis of certain flight parameters based on MEMS sensors |
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