Engagement areas of missiles in the proportional navigated flight powered by air breathing engines
The goals of this research are to test the relationships of appropriate nonline of site (NLOS) missile flight performances and conditionally created their tactical ranges, spaces zones and shooting time during employment on the surface targets. Flight maneuver of distance remote controlled NLOS miss...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
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University of Belgrade - Faculty of Mechanical Engineering, Belgrade
2014-01-01
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| Series: | FME Transactions |
| Subjects: | |
| Online Access: | https://scindeks-clanci.ceon.rs/data/pdf/1451-2092/2014/1451-20921403181M.pdf |
| _version_ | 1818996416023887872 |
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| author | Marković Miloš Rašuo Boško Milinović Momčilo Amine Mohammed Boulahlib |
| author_facet | Marković Miloš Rašuo Boško Milinović Momčilo Amine Mohammed Boulahlib |
| author_sort | Marković Miloš |
| collection | DOAJ |
| description | The goals of this research are to test the relationships of appropriate nonline of site (NLOS) missile flight performances and conditionally created their tactical ranges, spaces zones and shooting time during employment on the surface targets. Flight maneuver of distance remote controlled NLOS missile is tested with the conditionally joint constrains coming from flight kinematics with turbo-jet engine of NLOS missile and manner of target motion, typical of rapid reaction attacks. The constraints of maneuverability and flight, in the cruise phase, are considered as the mass point motion to create both unguided (searching) and guided navigated kinematical trajectories, which was designed by the appropriate guidance law. Research used numerical methods to simulate NLOS missile and targets motions in horizontal plane by controlling line of target (LOT) referred at the appropriate flight height. This generates borders of target impact and launching areas, establishes NLOS missile operation time, as well as masses variations for the expected manner of battle flight. . |
| first_indexed | 2024-12-20T21:29:23Z |
| format | Article |
| id | doaj.art-4ba0760ef3fd47119514e2f2f21a2751 |
| institution | Directory Open Access Journal |
| issn | 1451-2092 2406-128X |
| language | English |
| last_indexed | 2024-12-20T21:29:23Z |
| publishDate | 2014-01-01 |
| publisher | University of Belgrade - Faculty of Mechanical Engineering, Belgrade |
| record_format | Article |
| series | FME Transactions |
| spelling | doaj.art-4ba0760ef3fd47119514e2f2f21a27512022-12-21T19:26:05ZengUniversity of Belgrade - Faculty of Mechanical Engineering, BelgradeFME Transactions1451-20922406-128X2014-01-014231811881451-20921403181MEngagement areas of missiles in the proportional navigated flight powered by air breathing enginesMarković Miloš0Rašuo Boško1https://orcid.org/0000-0002-0912-6844Milinović Momčilo2https://orcid.org/0000-0002-5361-7544Amine Mohammed Boulahlib3University of Belgrade, Faculty of Mechanical EngineeringUniversity of Belgrade, Faculty of Mechanical EngineeringUniversity of Belgrade, Faculty of Mechanical EngineeringMinistry of National Defence, AlgeriaThe goals of this research are to test the relationships of appropriate nonline of site (NLOS) missile flight performances and conditionally created their tactical ranges, spaces zones and shooting time during employment on the surface targets. Flight maneuver of distance remote controlled NLOS missile is tested with the conditionally joint constrains coming from flight kinematics with turbo-jet engine of NLOS missile and manner of target motion, typical of rapid reaction attacks. The constraints of maneuverability and flight, in the cruise phase, are considered as the mass point motion to create both unguided (searching) and guided navigated kinematical trajectories, which was designed by the appropriate guidance law. Research used numerical methods to simulate NLOS missile and targets motions in horizontal plane by controlling line of target (LOT) referred at the appropriate flight height. This generates borders of target impact and launching areas, establishes NLOS missile operation time, as well as masses variations for the expected manner of battle flight. .https://scindeks-clanci.ceon.rs/data/pdf/1451-2092/2014/1451-20921403181M.pdfshooting arearange performancesproportional navigationendurance of flightnon-line of site missile |
| spellingShingle | Marković Miloš Rašuo Boško Milinović Momčilo Amine Mohammed Boulahlib Engagement areas of missiles in the proportional navigated flight powered by air breathing engines FME Transactions shooting area range performances proportional navigation endurance of flight non-line of site missile |
| title | Engagement areas of missiles in the proportional navigated flight powered by air breathing engines |
| title_full | Engagement areas of missiles in the proportional navigated flight powered by air breathing engines |
| title_fullStr | Engagement areas of missiles in the proportional navigated flight powered by air breathing engines |
| title_full_unstemmed | Engagement areas of missiles in the proportional navigated flight powered by air breathing engines |
| title_short | Engagement areas of missiles in the proportional navigated flight powered by air breathing engines |
| title_sort | engagement areas of missiles in the proportional navigated flight powered by air breathing engines |
| topic | shooting area range performances proportional navigation endurance of flight non-line of site missile |
| url | https://scindeks-clanci.ceon.rs/data/pdf/1451-2092/2014/1451-20921403181M.pdf |
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