GBAS-based high-precision automatic landing guidance for civil aircraft using improved active disturbance rejection control
GBAS landing system (GLS) serves as an effective means to enhance the accuracy and efficiency of approach and landing, and it is recognized as an essential function for modern and future advanced civil aircraft onboard avionics systems. This article presents a high-precision three-dimensional GLS ap...
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| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
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Elsevier
2025-09-01
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| Series: | Results in Engineering |
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| Online Access: | http://www.sciencedirect.com/science/article/pii/S2590123025017876 |
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| _version_ | 1849685797480955904 |
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| author | Shaobo Zhai Guangwen Li Junmin Cheng Mingshan Hou |
| author_facet | Shaobo Zhai Guangwen Li Junmin Cheng Mingshan Hou |
| author_sort | Shaobo Zhai |
| collection | DOAJ |
| description | GBAS landing system (GLS) serves as an effective means to enhance the accuracy and efficiency of approach and landing, and it is recognized as an essential function for modern and future advanced civil aircraft onboard avionics systems. This article presents a high-precision three-dimensional GLS approach guidance algorithm. Specifically, a spatial geometric relationship-based guidance deviation calculation method and a distance correction strategy-based guidance commands generation method are developed. Subsequently, an improved active disturbance rejection control method using the sine-function is proposed to design the robust attitude controller, ensuring precise tracking of the guidance commands. Through simulations, the algorithms are verified using Monte Carlo method, and the results showcase that the proposed algorithms can provide gratifying approach and guidance capability even with wind interference, sensor noise, and model parameter uncertainties. |
| format | Article |
| id | doaj-art-e8bf02a23a434a54983d4bc3e59b5bea |
| institution | DOAJ |
| issn | 2590-1230 |
| language | English |
| publishDate | 2025-09-01 |
| publisher | Elsevier |
| record_format | Article |
| series | Results in Engineering |
| spelling | doaj-art-e8bf02a23a434a54983d4bc3e59b5bea2025-08-20T03:22:58ZengElsevierResults in Engineering2590-12302025-09-012710571610.1016/j.rineng.2025.105716GBAS-based high-precision automatic landing guidance for civil aircraft using improved active disturbance rejection controlShaobo Zhai0Guangwen Li1Junmin Cheng2Mingshan Hou3School of Automation, Northwestern Polytechnical University, Xi’an 710072, ChinaCorresponding author.; School of Automation, Northwestern Polytechnical University, Xi’an 710072, ChinaSchool of Automation, Northwestern Polytechnical University, Xi’an 710072, ChinaSchool of Automation, Northwestern Polytechnical University, Xi’an 710072, ChinaGBAS landing system (GLS) serves as an effective means to enhance the accuracy and efficiency of approach and landing, and it is recognized as an essential function for modern and future advanced civil aircraft onboard avionics systems. This article presents a high-precision three-dimensional GLS approach guidance algorithm. Specifically, a spatial geometric relationship-based guidance deviation calculation method and a distance correction strategy-based guidance commands generation method are developed. Subsequently, an improved active disturbance rejection control method using the sine-function is proposed to design the robust attitude controller, ensuring precise tracking of the guidance commands. Through simulations, the algorithms are verified using Monte Carlo method, and the results showcase that the proposed algorithms can provide gratifying approach and guidance capability even with wind interference, sensor noise, and model parameter uncertainties.http://www.sciencedirect.com/science/article/pii/S2590123025017876GBAS landing systemThree-dimensional approach guidanceSpatial geometric relationshipDistance correction strategyActive disturbance rejection control |
| spellingShingle | Shaobo Zhai Guangwen Li Junmin Cheng Mingshan Hou GBAS-based high-precision automatic landing guidance for civil aircraft using improved active disturbance rejection control Results in Engineering GBAS landing system Three-dimensional approach guidance Spatial geometric relationship Distance correction strategy Active disturbance rejection control |
| title | GBAS-based high-precision automatic landing guidance for civil aircraft using improved active disturbance rejection control |
| title_full | GBAS-based high-precision automatic landing guidance for civil aircraft using improved active disturbance rejection control |
| title_fullStr | GBAS-based high-precision automatic landing guidance for civil aircraft using improved active disturbance rejection control |
| title_full_unstemmed | GBAS-based high-precision automatic landing guidance for civil aircraft using improved active disturbance rejection control |
| title_short | GBAS-based high-precision automatic landing guidance for civil aircraft using improved active disturbance rejection control |
| title_sort | gbas based high precision automatic landing guidance for civil aircraft using improved active disturbance rejection control |
| topic | GBAS landing system Three-dimensional approach guidance Spatial geometric relationship Distance correction strategy Active disturbance rejection control |
| url | http://www.sciencedirect.com/science/article/pii/S2590123025017876 |
| work_keys_str_mv | AT shaobozhai gbasbasedhighprecisionautomaticlandingguidanceforcivilaircraftusingimprovedactivedisturbancerejectioncontrol AT guangwenli gbasbasedhighprecisionautomaticlandingguidanceforcivilaircraftusingimprovedactivedisturbancerejectioncontrol AT junmincheng gbasbasedhighprecisionautomaticlandingguidanceforcivilaircraftusingimprovedactivedisturbancerejectioncontrol AT mingshanhou gbasbasedhighprecisionautomaticlandingguidanceforcivilaircraftusingimprovedactivedisturbancerejectioncontrol |