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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Main Author: Laurentiu MORARU
Format: Article
Language:English
Published: National Institute for Aerospace Research “Elie Carafoli” - INCAS 2015-09-01
Series:INCAS Bulletin
Subjects:
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.
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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
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