Navigation Aids Performance Evaluation for Precision Approaches

The paper deals with the evaluation of the expected performance of aircraft approaches and landings operated with different navigation systems, both traditional and satellite-based. Flight dynamics characteristics and control authority of the approaching aircraft are considered in order to obtain an...

Full description

Bibliographic Details
Main Authors: Pier Domenico Tromboni, Giovanni B. Palmerini
Format: Article
Language:English
Published: Hindawi Limited 2010-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2010/389832
id doaj-85d425bba6bc4486aebbad5aacf816de
record_format Article
spelling doaj-85d425bba6bc4486aebbad5aacf816de2020-11-24T21:04:21ZengHindawi LimitedInternational Journal of Aerospace Engineering1687-59661687-59742010-01-01201010.1155/2010/389832389832Navigation Aids Performance Evaluation for Precision ApproachesPier Domenico Tromboni0Giovanni B. Palmerini1Università degli studi di Roma “La Sapienza”, via Eudossiana, 18-00184 Roma, ItalyUniversità degli studi di Roma “La Sapienza”, via Eudossiana, 18-00184 Roma, ItalyThe paper deals with the evaluation of the expected performance of aircraft approaches and landings operated with different navigation systems, both traditional and satellite-based. Flight dynamics characteristics and control authority of the approaching aircraft are considered in order to obtain an overall manoeuvre evaluation. The technique from the presented analysis applies to different operative conditions, taking into account aircraft requirements, navigation systems features, and environmental constraints. The aim is to offer a tool to be used in the very preliminary design phase for system performance analysis in different scenarios, such as airport ground systems adoption and air traffic control requirements compliance; later, the same tool can be tuned to complement and direct the required real flight trials to validate an already fielded solution. A numerical code referring to the presented analytical model has been implemented and some applications concerning the system's performance evaluation and planning are proposed to illustrate the algorithm capabilities. The tool and the proposed analysis technique indeed are successful in providing a quantitative assessment of the differences among several possible approaches.http://dx.doi.org/10.1155/2010/389832
collection DOAJ
language English
format Article
sources DOAJ
author Pier Domenico Tromboni
Giovanni B. Palmerini
spellingShingle Pier Domenico Tromboni
Giovanni B. Palmerini
Navigation Aids Performance Evaluation for Precision Approaches
International Journal of Aerospace Engineering
author_facet Pier Domenico Tromboni
Giovanni B. Palmerini
author_sort Pier Domenico Tromboni
title Navigation Aids Performance Evaluation for Precision Approaches
title_short Navigation Aids Performance Evaluation for Precision Approaches
title_full Navigation Aids Performance Evaluation for Precision Approaches
title_fullStr Navigation Aids Performance Evaluation for Precision Approaches
title_full_unstemmed Navigation Aids Performance Evaluation for Precision Approaches
title_sort navigation aids performance evaluation for precision approaches
publisher Hindawi Limited
series International Journal of Aerospace Engineering
issn 1687-5966
1687-5974
publishDate 2010-01-01
description The paper deals with the evaluation of the expected performance of aircraft approaches and landings operated with different navigation systems, both traditional and satellite-based. Flight dynamics characteristics and control authority of the approaching aircraft are considered in order to obtain an overall manoeuvre evaluation. The technique from the presented analysis applies to different operative conditions, taking into account aircraft requirements, navigation systems features, and environmental constraints. The aim is to offer a tool to be used in the very preliminary design phase for system performance analysis in different scenarios, such as airport ground systems adoption and air traffic control requirements compliance; later, the same tool can be tuned to complement and direct the required real flight trials to validate an already fielded solution. A numerical code referring to the presented analytical model has been implemented and some applications concerning the system's performance evaluation and planning are proposed to illustrate the algorithm capabilities. The tool and the proposed analysis technique indeed are successful in providing a quantitative assessment of the differences among several possible approaches.
url http://dx.doi.org/10.1155/2010/389832
work_keys_str_mv AT pierdomenicotromboni navigationaidsperformanceevaluationforprecisionapproaches
AT giovannibpalmerini navigationaidsperformanceevaluationforprecisionapproaches
_version_ 1716771412319928320