An Expedite Approximate Algorithm for Calculating the Controls in the Longitudinal Maneuver
This paper discusses an expedite approximate algorithm for obtaining the controls in the longitudinal maneuver of the aerospace vehicles. The equations of motion are written in terms of the flight path (the trajectory that is desired is also given in terms of flight path, that is the local radius of...
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Format: | Article |
Language: | English |
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National Institute for Aerospace Research “Elie Carafoli” - INCAS
2015-09-01
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Series: | INCAS Bulletin |
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Online Access: | http://bulletin.incas.ro/files/moraru_vol_7_iss_3.pdf |
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author | Laurentiu MORARU |
author_facet | Laurentiu MORARU |
author_sort | Laurentiu MORARU |
collection | DOAJ |
description | This paper discusses an expedite approximate algorithm for obtaining the controls in the longitudinal maneuver of the aerospace vehicles. The equations of motion are written in terms of the flight path (the trajectory that is desired is also given in terms of flight path, that is the local radius of curvature is given as a function of flight path) and the controls required for following a desired trajectory obtained accordingly. A finite terms integration procedure is subsequently presented. |
first_indexed | 2024-12-17T10:46:39Z |
format | Article |
id | doaj.art-e4d786621ed4404a88d4d89e69105cff |
institution | Directory Open Access Journal |
issn | 2066-8201 2247-4528 |
language | English |
last_indexed | 2024-12-17T10:46:39Z |
publishDate | 2015-09-01 |
publisher | National Institute for Aerospace Research “Elie Carafoli” - INCAS |
record_format | Article |
series | INCAS Bulletin |
spelling | doaj.art-e4d786621ed4404a88d4d89e69105cff2022-12-21T21:52:06ZengNational Institute for Aerospace Research “Elie Carafoli” - INCASINCAS Bulletin2066-82012247-45282015-09-017312112810.13111/2066-8201.2015.7.3.11An Expedite Approximate Algorithm for Calculating the Controls in the Longitudinal ManeuverLaurentiu MORARU0“POLITEHNICA” University of Bucharest, Department of Aerospace Sciences Splaiul Independenţei 313, 060042, Bucharest, Romania laurentiu.moraru@gmail.comThis paper discusses an expedite approximate algorithm for obtaining the controls in the longitudinal maneuver of the aerospace vehicles. The equations of motion are written in terms of the flight path (the trajectory that is desired is also given in terms of flight path, that is the local radius of curvature is given as a function of flight path) and the controls required for following a desired trajectory obtained accordingly. A finite terms integration procedure is subsequently presented.http://bulletin.incas.ro/files/moraru_vol_7_iss_3.pdfFlight Dynamics SimulationControlsLongitudinal |
spellingShingle | Laurentiu MORARU An Expedite Approximate Algorithm for Calculating the Controls in the Longitudinal Maneuver INCAS Bulletin Flight Dynamics Simulation Controls Longitudinal |
title | An Expedite Approximate Algorithm for Calculating the Controls in the Longitudinal Maneuver |
title_full | An Expedite Approximate Algorithm for Calculating the Controls in the Longitudinal Maneuver |
title_fullStr | An Expedite Approximate Algorithm for Calculating the Controls in the Longitudinal Maneuver |
title_full_unstemmed | An Expedite Approximate Algorithm for Calculating the Controls in the Longitudinal Maneuver |
title_short | An Expedite Approximate Algorithm for Calculating the Controls in the Longitudinal Maneuver |
title_sort | expedite approximate algorithm for calculating the controls in the longitudinal maneuver |
topic | Flight Dynamics Simulation Controls Longitudinal |
url | http://bulletin.incas.ro/files/moraru_vol_7_iss_3.pdf |
work_keys_str_mv | AT laurentiumoraru anexpediteapproximatealgorithmforcalculatingthecontrolsinthelongitudinalmaneuver AT laurentiumoraru expediteapproximatealgorithmforcalculatingthecontrolsinthelongitudinalmaneuver |