Anti-Collision System for Small Civil Aircraft
This paper presents the results of the research in the field of anti-collision systems for small civil aircraft, which are not dependent on secondary radars and satellite navigation systems. The aviation communication network was used to design the anti-collision system. The simulation results manif...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
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MDPI AG
2022-02-01
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| Series: | Applied Sciences |
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| Online Access: | https://www.mdpi.com/2076-3417/12/3/1648 |
| _version_ | 1797488975889301504 |
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| author | Milan Džunda Peter Dzurovčin Lucia Melníková |
| author_facet | Milan Džunda Peter Dzurovčin Lucia Melníková |
| author_sort | Milan Džunda |
| collection | DOAJ |
| description | This paper presents the results of the research in the field of anti-collision systems for small civil aircraft, which are not dependent on secondary radars and satellite navigation systems. The aviation communication network was used to design the anti-collision system. The simulation results manifested that the anti-collision system precision depended on the errors of synchronization of the aviation communication network. The precision of the anti-collision system is also influenced by the errors of the coordinates of individual aviation communication network users, based on which the system identifies its own position. The results of the simulation show that the dispersion of the positioning error σ<sup>2</sup><sub>∆P</sub> by the ACS system varied in the range of 1.94 m<sup>2</sup> to 503.23 m<sup>2</sup>. The simulation results confirm that the designed anti-collision system is operational in establishing its position against other FOs, with the distance from the given FOs being 50.0 km maximum. The main contribution of this paper are derived algorithms for the operation of an anti-collision system for small civil aircraft, in addition to the design of movement trajectory models of five flying objects which operate within the aviation communication network. The advantage of the anti-collision system is that it is independent of satnav systems and secondary radars. A significant advantage is the low cost of this system. |
| first_indexed | 2024-03-10T00:09:56Z |
| format | Article |
| id | doaj.art-383a196b40dc4bb7a9c333984b5c9359 |
| institution | Directory Open Access Journal |
| issn | 2076-3417 |
| language | English |
| last_indexed | 2024-03-10T00:09:56Z |
| publishDate | 2022-02-01 |
| publisher | MDPI AG |
| record_format | Article |
| series | Applied Sciences |
| spelling | doaj.art-383a196b40dc4bb7a9c333984b5c93592023-11-23T16:01:07ZengMDPI AGApplied Sciences2076-34172022-02-01123164810.3390/app12031648Anti-Collision System for Small Civil AircraftMilan Džunda0Peter Dzurovčin1Lucia Melníková2Department of Air Transport Management, Faculty of Aeronautics, Technical University of Košice, 040 01 Košice, SlovakiaDepartment of Air Transport Management, Faculty of Aeronautics, Technical University of Košice, 040 01 Košice, SlovakiaDepartment of Air Transport Management, Faculty of Aeronautics, Technical University of Košice, 040 01 Košice, SlovakiaThis paper presents the results of the research in the field of anti-collision systems for small civil aircraft, which are not dependent on secondary radars and satellite navigation systems. The aviation communication network was used to design the anti-collision system. The simulation results manifested that the anti-collision system precision depended on the errors of synchronization of the aviation communication network. The precision of the anti-collision system is also influenced by the errors of the coordinates of individual aviation communication network users, based on which the system identifies its own position. The results of the simulation show that the dispersion of the positioning error σ<sup>2</sup><sub>∆P</sub> by the ACS system varied in the range of 1.94 m<sup>2</sup> to 503.23 m<sup>2</sup>. The simulation results confirm that the designed anti-collision system is operational in establishing its position against other FOs, with the distance from the given FOs being 50.0 km maximum. The main contribution of this paper are derived algorithms for the operation of an anti-collision system for small civil aircraft, in addition to the design of movement trajectory models of five flying objects which operate within the aviation communication network. The advantage of the anti-collision system is that it is independent of satnav systems and secondary radars. A significant advantage is the low cost of this system.https://www.mdpi.com/2076-3417/12/3/1648anti-collision systemflying objectaccuracyaviation communication network |
| spellingShingle | Milan Džunda Peter Dzurovčin Lucia Melníková Anti-Collision System for Small Civil Aircraft Applied Sciences anti-collision system flying object accuracy aviation communication network |
| title | Anti-Collision System for Small Civil Aircraft |
| title_full | Anti-Collision System for Small Civil Aircraft |
| title_fullStr | Anti-Collision System for Small Civil Aircraft |
| title_full_unstemmed | Anti-Collision System for Small Civil Aircraft |
| title_short | Anti-Collision System for Small Civil Aircraft |
| title_sort | anti collision system for small civil aircraft |
| topic | anti-collision system flying object accuracy aviation communication network |
| url | https://www.mdpi.com/2076-3417/12/3/1648 |
| work_keys_str_mv | AT milandzunda anticollisionsystemforsmallcivilaircraft AT peterdzurovcin anticollisionsystemforsmallcivilaircraft AT luciamelnikova anticollisionsystemforsmallcivilaircraft |