Disseny d'un simulador de vol A320
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Inclou dades d'ús des de 2022
Cita com:
hdl:2099.1/9706
Tipus de documentProjecte/Treball Final de Carrera
Data2004-09-06
Condicions d'accésAccés restringit per decisió de l'autor
Tots els drets reservats. Aquesta obra està protegida pels drets de propietat intel·lectual i
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Abstract
The aim of this project is to study the viability of two avionics simulation
cockpits that are expected to be placed in an aeronautics laboratory in the near
future: a lightweight simple-engine aircraft simulator with a simple panel
(Cessna 152) and a multi-engine commercial aircraft simulator with a modern
panel and an automated flight management (Airbus-type). The Cessna’s cockpit is a general aviation cockpit, generally used to private
flights or training flights. It is a two-seater aircraft and the size of its cockpit is
similar to a car’s interior. The instrumentation found in a Cessna is very basic
and absolutely analogical, since it is an aircraft produced in the mid-sixties and
designed basically to do visual training flights.
Airbus is a more modern aircraft produced in the late eighties and designed
completely to commercial aviation. This kind of aircraft is able to transport more
than two hundred passengers and it is also able to jump long distances. The
cockpit is absolutely equipped with instruments (it is possible to take off and to
land even without looking outside the aircraft) and the interaction between the
crew and on board aeronavegation computers play a very decisive role.
This study considers different flight simulator softwares in order to obtain
the highest output from them, according to this project requirements. The three
most important flight simulators of the market are analized and both cockpits are
studied individually, by using the real operating manual of each aircraft. Two
summaries directed at their programming are also included: a summary of the
system and a specific summary.
This project considers neither the carrying out of graphic environment of the
simulator nor flight mechanics. These parameters are not supposed to provide
anything interesting to the school. What will be also done is a minucious study of
the structure the different simulators should have to get a successful
communication between computers, systems and users.
A project including the whole UPC is proposed, having into account that all
future investigators will not be aeronautical engineers. Several supporting
documents are added to this paper in order to help different non-aeronautical
engineers to work on this project. Finally, different related projects and their
explanations are proposed to further this investigation.
TitulacióENGINYERIA TÈCNICA DE TELECOMUNICACIÓ, ESPECIALITAT EN SISTEMES DE TELECOMUNICACIÓ (Pla 2000)
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memoria.pdf | Memòria | 4,375Mb | Accés restringit |