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dc.contributorLizandra Dalmases, José Oriol
dc.contributor.authorSanches, Leonardo
dc.contributor.otherUniversitat Politècnica de Catalunya. Departament d'Enginyeria de Sistemes, Automàtica i Informàtica Industrial
dc.date.accessioned2008-01-07T09:50:07Z
dc.date.available2008-01-07T09:50:07Z
dc.date.issued2007-06
dc.identifier.urihttp://hdl.handle.net/2099.1/4494
dc.description.abstractThe development of closed loop control has been one of the major technological achievements of the twentieth century, and its concepts married with analogue and digital computation led to explosive growth in the sophistication of the technology and the ubiquity of its application. By that, an automatic flight control system is able to stabilize an inherently unstable airplane or to provide a stability augmentation system (SAS). In other words, there is no margin for error in its response to atmospheric disturbances and to commands that come from navigation system. Moreover it improves the handling qualities, the flight comfort and reduces the costs when an airplane is under control of an autopilot. This specific project is destined to simulate and analyze the operating parameters (i.e., altitude, pitch angle, airspeed, throttle level, and elevator angle) of a passenger aircraft - Boeing 747-100 –in longitudinal motion deflected from its ordered flight trajectory and atmospheric condition when related with its reference steady flight parameters. For all cases studied, the results are satisfactory controlled and expected. Future works can be done in using the differential equations instead of linearized ones, which increases the range of possible cases to be studied.
dc.language.isoeng
dc.publisherUniversitat Politècnica de Catalunya
dc.subjectÀrees temàtiques de la UPC::Aeronàutica i espai::Aeronaus
dc.subject.lcshAircraft industry Research
dc.subject.lcshFlight simulators
dc.titleStudy and Simulation of Dynamic Longitudinal Stability of a Passenger Aircraft –Boeing 747-100- on Adverse Atmosphere Conditions
dc.typeMaster thesis
dc.subject.lemacAeronaus -- Métodes de simulació
dc.subject.lemacSimuladors de vol
dc.rights.accessOpen Access
dc.audience.educationlevelMàster
dc.audience.mediatorEscola Tècnica Superior d'Enginyeria Industrial de Barcelona
dc.provenanceAquest document conté originàriament altre material i/o programari no inclòs en aquest lloc web


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