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- W4313196133 abstract "During aircraft approach and landing, localizer and glideslope signals of the Instrument Landing System (ILS) is susceptible to electromagnetic interference from other aircraft in the airport airspace and the ground environment, affecting the landing guidance accuracy and even causing misguided guidance. In this paper, a new method based on ILS and other airborne sensors such as INS (Inertial Navigation System), GPS (Global Position System), and RA (Radar Altimeter) to calculate the localizer and glideslope deviation of the aircraft relative to the reference landing trajectory is proposed. The localizer and glideslope deviation angle of the aircraft are measured by the ILS, and the three-dimensional position information of the aircraft is obtained by combining the measurement with the DME(Distance Measurement Equipment), using the Kalman filter to estimate and correct the localizer and glideslope deviation errors to obtain the initial deviation when ILS is not disturbed, and then obtain the rate of the localizer and glideslope deviation from the INS/GPS/RA integrated navigation system, and finally synthesize the virtual localizer and glideslope deviation once the signals of ILS are abnormal. The simulation results show that the proposed method can effectively improve the accuracy and reliability of the landing guidance signals in the disturbed landing scenario." @default.
- W4313196133 created "2023-01-06" @default.
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- W4313196133 date "2022-01-01" @default.
- W4313196133 modified "2023-09-27" @default.
- W4313196133 title "Virtual synthesis method on the localizer and glideslope guidance signal for instrument landing system" @default.
- W4313196133 doi "https://doi.org/10.1049/icp.2022.1848" @default.
- W4313196133 hasPublicationYear "2022" @default.
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