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Managing aircraft noise彭遠輝, Pang, Yuen-fai, Alson. January 2002 (has links)
published_or_final_version / Environmental Management / Master / Master of Science in Environmental Management
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The effect of flight deck automation and automation proficiency on cockpit task management performanceSuroteguh, Candy Brodie 30 August 1999 (has links)
Piloting a commercial aircraft involves performing multiple tasks in a real-time
environment that require pilot's attention and cognitive resource allocation. Due to resource
limitation, pilots must perform cockpit task management (CTM) because they cannot perform
all tasks that demand their attention at once. Hence, pilots must prioritize the tasks in the order
of most to least important and allocate their resources according to this prioritization.
Over the years, pilots have developed rules of thumb for task prioritization in
facilitating CTM. A task prioritization error is simply an error made by the flight crew when
they perform lower priority tasks as opposed to higher priority tasks, where priority is
determined by the Aviate-Navigate-Communicate-Manage Systems (A-N-C-S) task ordering.
Although the level of flight deck automation has been suggested as one factor
influencing the likelihood of task prioritization errors, there has so far been just one study
directed towards confirming that hypothesis. Hence the first objective of this study was to
determine the effect of the level of automation on CTM performance. CTM performance was
measured by looking at the number of task prioritization errors committed by pilots in
different levels of automation. In addition to the level of automation, there was also reason to
believe that the pilot's automation proficiency might affect CTM performance. Therefore, the
second objective of this study was to determine the effect of automation proficiency on CTM
performance.
Nine airline transport pilots served as subjects in this study. Three flying scenarios
and three levels of flight deck automation were simulated on a part-task flight simulator. Each
pilot ran three different combinations of flight deck automation and flying scenario. The CTM
performance for each pilot was determined by identifying the number of task prioritization
errors committed in each experiment run. The average number of errors in different levels of
automation and automation proficiency were compared for their effect on CTM performance
using Analysis of Variance (ANOVA). It was found that the level of automation affected
CTM performance depending scenarios in which phases of flight differed. However,
automation proficiency, measured by glass cockpit hours, was found to have no effect on
CTM performance. / Graduation date: 2000
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An agent-based cockpit task management system : a task-oriented pilot-vehicle interfaceKim, Joong Nam 17 November 1994 (has links)
Graduation date: 1995
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Adaptive nonlinear flight controlRysdyk, Rolf T. 12 1900 (has links)
No description available.
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Aircraft noise and public health : acoustical measurement and social survey around Sydney, Kingsford Smith Airport /Issarayangyun, Tharit. January 2005 (has links)
Thesis (Ph. D.)--University of New South Wales, 2005. / Also available online.
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Aircraft control with nonlinear indicial response modelCetek, Cem. January 1999 (has links)
Thesis (M.S.)--Ohio University, March, 1999. / Title from PDF t.p.
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Demonstrative maneuvers for aircraft agility predictions /Hall, David M. January 2008 (has links) (PDF)
Thesis (M.S. in in Aeronautical Engineering)--Air Force Institute of Technology, March 2008. / "Presented to the Faculty, Department of Aeronautics and Astronautics Graduate School of Engineering and Management, Air Force Institute of Technology Air University, Air Education and Training Command in partial fulfillment of the requirements for the Degree of Master of Science in Aeronautical Engineering, March 2008."--P. [ii]. Thesis advisor: Lt. Col. Chris Shearer. "March 2008." "AFIT/GAE/ENY/08-M13." Includes bibliographical references. Also available online in PDF from the DTIC Online Web site.
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Design recovery and implementation of the AYK-14 VHSIC processor module adapter with field programmable gate array technology /Fetter, Bryan J. January 2002 (has links) (PDF)
Thesis (M.S. in Aeronautical Engineering)--Naval Postgraduate School, December 2002. / Thesis advisor(s): Russell W. Duren, Hersch Loomis. Includes bibliographical references (p. 199). Also available online.
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Development of deployable wings for small unmanned aerial vehicles using compliant mechanisms /Landon, Steven D., January 2007 (has links) (PDF)
Thesis (M.S.)--Brigham Young University. Dept. of Mechanical Engineering, 2007. / Includes bibliographical references (p. 113-116).
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Numerical analysis of plane cracks in strain-gradient elastic materialsAkarapu, Sreekanth, January 2005 (has links) (PDF)
Thesis (M.S.)--Washington State University, December 2005. / Includes bibliographical references.
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