International Journal For Multidisciplinary Research

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Analysis of the Stability Augmentation System of an Aircraft (SJ30) in Flight Turbulence

Author(s) David Laud Amenyo Fiase, Kwawdo Opoku Attah, Prince Sackey, Freda Ocansey, Samuel Lartey
Country Ghana
Abstract The article analyzed the Stability Augmentation System (yaw damping) of Syberjet 30 aircraft in turbulent conditions using High Level programming Language. The yaw damper significantly reduced the short-period lateral-directional motion of the aircraft in turbulent air resulting in both the ride and the flying qualities. There was no significant improvement in the pilot’s overall performance of the Instrument Landing System (ILS) approach task. The aileron-to-rudder interconnect was found to be effective in compensating for adverse aileron yaw and turns could be made easier and more accurately. An increase in the intensity of the lateral motions of the airplane in turbulent was experienced when the autopilot system was used alone. The autopilot performance in turbulent was significantly improved when the system was used with the yaw damper. It will therefore be recommendable to the aeronautical sector to use the yaw damper to improve the autopilot performance in turbulence.
Keywords Instrument Landing System (ILS), Stability Augmentation System (SAS), Yaw Damping, Autopilot, Control Augmentation system (CAS), Automatic Control System (ACS)
Field Engineering
Published In Volume 6, Issue 3, May-June 2024
Published On 2024-06-10
Cite This Analysis of the Stability Augmentation System of an Aircraft (SJ30) in Flight Turbulence - David Laud Amenyo Fiase, Kwawdo Opoku Attah, Prince Sackey, Freda Ocansey, Samuel Lartey - IJFMR Volume 6, Issue 3, May-June 2024. DOI 10.36948/ijfmr.2024.v06i03.19290
DOI https://doi.org/10.36948/ijfmr.2024.v06i03.19290
Short DOI https://doi.org/gtzjqz
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