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Simulation and Evaluation of Civil Aircraft Auto-Landing with Various Guidance Systems

  • Beihang University

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

Abstract

The goal of this study is to discuss the role of different guidance systems during landing phase facing preliminary design of large civil aircraft landing system. As a basic, an auto-landing control system of Boeing 747 is designed. Based on the signal statistics of ILS, GPS, radar system and the image-forming principle of visual guidance system, the four guidance error models are established. Then a method of evaluating the guidance systems is put forward by defining safety cost and comfort cost according to performance indexes. Finally, simulations of auto-landing are performed to evaluate performance of guidance systems and a design-making progress is designed. The results can reflect the characteristics of different guidance systems and help to analysis the guidance strategy for information fusion.

Original languageEnglish
Title of host publicationProceedings of 2018 9th International Conference on Mechanical and Aerospace Engineering, ICMAE 2018
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages238-242
Number of pages5
ISBN (Electronic)9781538672297
DOIs
StatePublished - 18 Sep 2018
Event9th International Conference on Mechanical and Aerospace Engineering, ICMAE 2018 - Budapest, Hungary
Duration: 10 Jul 2018 → 13 Jul 2018

Publication series

NameProceedings of 2018 9th International Conference on Mechanical and Aerospace Engineering, ICMAE 2018

Conference

Conference9th International Conference on Mechanical and Aerospace Engineering, ICMAE 2018
Country/TerritoryHungary
CityBudapest
Period10/07/18 → 13/07/18

Keywords

  • GPS
  • ILS
  • auto-landing
  • civil aircraft
  • radar
  • visual guidance

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