Development Steps of Avionics and Flight Control System of Flight Vehicle
The success of a research is highly dependent on the method adopted, especially research related to dangerous and expensive matters which will certainly require special handling in the development or maintenance steps. One of them is research related to space technology such as aviation and rocketry...
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| Format: | Article |
| Language: | English |
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Ikatan Ahli Informatika Indonesia
2023-08-01
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| Series: | Jurnal RESTI (Rekayasa Sistem dan Teknologi Informasi) |
| Subjects: | |
| Online Access: | http://jurnal.iaii.or.id/index.php/RESTI/article/view/4953 |
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| author | Herma Yudhi Irwanto Purnomo Yusgiantoro Zainal Abidin Sahabuddin Romie Oktovianus Bura Aris Sarjito Oka Sudiana Faisa Lailiyul Mutho' Affifah |
| author_facet | Herma Yudhi Irwanto Purnomo Yusgiantoro Zainal Abidin Sahabuddin Romie Oktovianus Bura Aris Sarjito Oka Sudiana Faisa Lailiyul Mutho' Affifah |
| author_sort | Herma Yudhi Irwanto |
| collection | DOAJ |
| description | The success of a research is highly dependent on the method adopted, especially research related to dangerous and expensive matters which will certainly require special handling in the development or maintenance steps. One of them is research related to space technology such as aviation and rocketry technology, which is very dependent on the design model of the flying vehicle and, in general, will always use simulation to ensure that the entire system being built is carried out safely and can be implemented properly according to plan. In the development of the prototype flying vehicle, especially the development of the avionics and flight control system, the vehicle will go through sequential simulation steps from Software in the Loop Simulation (SILS), Hardware in the Loop Simulation (HILS), and Ready-to-Fly System (RTFS). In this paper, the simulation steps will be described with the intention of facilitating integration and testing of each sub-system being developed, testing the control strategy applied or eliminating bugs if something goes wrong. In the end, with a series of flying vehicle simulations, it can be developed quickly and cost-effectively, including saving human resources. |
| first_indexed | 2024-03-08T06:32:01Z |
| format | Article |
| id | doaj.art-1f07c8ba9c72453a82f622e9ed04606a |
| institution | Directory Open Access Journal |
| issn | 2580-0760 |
| language | English |
| last_indexed | 2024-03-08T06:32:01Z |
| publishDate | 2023-08-01 |
| publisher | Ikatan Ahli Informatika Indonesia |
| record_format | Article |
| series | Jurnal RESTI (Rekayasa Sistem dan Teknologi Informasi) |
| spelling | doaj.art-1f07c8ba9c72453a82f622e9ed04606a2024-02-03T11:19:18ZengIkatan Ahli Informatika IndonesiaJurnal RESTI (Rekayasa Sistem dan Teknologi Informasi)2580-07602023-08-017479179610.29207/resti.v7i4.49534953Development Steps of Avionics and Flight Control System of Flight VehicleHerma Yudhi Irwanto0Purnomo Yusgiantoro1Zainal Abidin Sahabuddin2Romie Oktovianus Bura3Aris Sarjito4Oka Sudiana5Faisa Lailiyul Mutho' Affifah6Badan Riset dan Inovasi NasionalUniversitas Pertahanan Republik IndonesiaUniversitas Pertahanan Republik IndonesiaUniversitas Pertahanan Republik IndonesiaUniversitas Pertahanan Republik IndonesiaBadan Riset dan Inovasi NasionalBadan Riset dan Inovasi NasionalThe success of a research is highly dependent on the method adopted, especially research related to dangerous and expensive matters which will certainly require special handling in the development or maintenance steps. One of them is research related to space technology such as aviation and rocketry technology, which is very dependent on the design model of the flying vehicle and, in general, will always use simulation to ensure that the entire system being built is carried out safely and can be implemented properly according to plan. In the development of the prototype flying vehicle, especially the development of the avionics and flight control system, the vehicle will go through sequential simulation steps from Software in the Loop Simulation (SILS), Hardware in the Loop Simulation (HILS), and Ready-to-Fly System (RTFS). In this paper, the simulation steps will be described with the intention of facilitating integration and testing of each sub-system being developed, testing the control strategy applied or eliminating bugs if something goes wrong. In the end, with a series of flying vehicle simulations, it can be developed quickly and cost-effectively, including saving human resources.http://jurnal.iaii.or.id/index.php/RESTI/article/view/4953software in the loop simulation (sils)hardware in the loop simulation (hils)ready to fly system (rtfs) |
| spellingShingle | Herma Yudhi Irwanto Purnomo Yusgiantoro Zainal Abidin Sahabuddin Romie Oktovianus Bura Aris Sarjito Oka Sudiana Faisa Lailiyul Mutho' Affifah Development Steps of Avionics and Flight Control System of Flight Vehicle Jurnal RESTI (Rekayasa Sistem dan Teknologi Informasi) software in the loop simulation (sils) hardware in the loop simulation (hils) ready to fly system (rtfs) |
| title | Development Steps of Avionics and Flight Control System of Flight Vehicle |
| title_full | Development Steps of Avionics and Flight Control System of Flight Vehicle |
| title_fullStr | Development Steps of Avionics and Flight Control System of Flight Vehicle |
| title_full_unstemmed | Development Steps of Avionics and Flight Control System of Flight Vehicle |
| title_short | Development Steps of Avionics and Flight Control System of Flight Vehicle |
| title_sort | development steps of avionics and flight control system of flight vehicle |
| topic | software in the loop simulation (sils) hardware in the loop simulation (hils) ready to fly system (rtfs) |
| url | http://jurnal.iaii.or.id/index.php/RESTI/article/view/4953 |
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