Evolution of Flying Qualities Analysis: Problems for a New Generation of Aircraft

dc.contributor.authorCotting, Malcolm Christopheren
dc.contributor.committeechairWoolsey, Craig A.en
dc.contributor.committeecochairDurham, Wayne C.en
dc.contributor.committeememberMcCue-Weil, Leigh S.en
dc.contributor.committeememberBordignon, Kenneth A.en
dc.contributor.committeememberMason, William H.en
dc.contributor.departmentAerospace and Ocean Engineeringen
dc.date.accessioned2014-03-14T20:09:24Zen
dc.date.adate2010-05-05en
dc.date.available2014-03-14T20:09:24Zen
dc.date.issued2010-03-29en
dc.date.rdate2010-05-05en
dc.date.sdate2010-04-11en
dc.description.abstractA number of challenges in the development and application of flying qualities criteria for modern aircraft are addressed in this dissertation. The history of flying qualities is traced from its origins to modern day techniques as applied to piloted aircraft. Included in this historical review is the case that was made for the development of flying qualities criteria in the 1940's and 1950's when piloted aircraft became prevalent in the United States military. It is then argued that UAVs today are in the same context historically as piloted aircraft when flying qualities criteria were first developed. To aid in development of a flying qualities criterion for UAVs, a relevant classification system for UAVs. Two longitudinal flying qualities criteria are developed for application to autonomous UAVs. These criteria center on mission performance of the integrated aircraft and sensor system. The first criterion is based on a sensor platform's ability to reject aircraft disturbances in pitch attitude. The second criterion makes use of energy methods to create a metric to quantify the transmission of turbulence to the sensor platform. These criteria are evaluated with airframe models of different classes of air vehicles using the CASTLE 6 DOF simulation. Another topic in flying qualities is the evaluation of nonlinear control systems in piloted aircraft. A L1 adaptive controller was implemented and tested in a motion based, piloted flight simulator. This is the first time that the L1 controller has been evaluated for piloted handling qualities. Results showed that the adaptive controller was able to recover good flying qualities from a degraded aircraft. The final topic addresses a less direct, but extremely important challenge for flying qualities research and education: a capstone course in flight mechanics teaching flight test techniques and featuring a motion based flight simulator was implemented and evaluated. The course used a mixture of problem based learning and role based learning to create an environment where students could explore key flight mechanics concepts. Evaluation of the course's effectiveness to promote the understanding of key flight mechanics concepts is presented.en
dc.description.degreePh. D.en
dc.identifier.otheretd-04112010-222856en
dc.identifier.sourceurlhttp://scholar.lib.vt.edu/theses/available/etd-04112010-222856/en
dc.identifier.urihttp://hdl.handle.net/10919/26781en
dc.publisherVirginia Techen
dc.relation.haspartCotting_MC_D_2010.pdfen
dc.rightsIn Copyrighten
dc.rights.urihttp://rightsstatements.org/vocab/InC/1.0/en
dc.subjectEducationen
dc.subjectFlight Mechanicsen
dc.subjectFlying Qualitiesen
dc.subjectDrone aircraften
dc.titleEvolution of Flying Qualities Analysis: Problems for a New Generation of Aircraften
dc.typeDissertationen
thesis.degree.disciplineAerospace and Ocean Engineeringen
thesis.degree.grantorVirginia Polytechnic Institute and State Universityen
thesis.degree.leveldoctoralen
thesis.degree.namePh. D.en
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