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You searched for subject:(Pilot induced oscillation). Showing records 1 – 5 of 5 total matches.

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Cranfield University

1. Lee, Brian P. Pilot and control system modelling for handling qualities analysis of large transport aircraft.

Degree: PhD, 2012, Cranfield University

 The notion of airplane stability and control being a balancing act between stability and control has been around as long as aeronautics. The Wright brothers’… (more)

Subjects/Keywords: Stability and control; Flight dynamics; Flying qualities; Pilot induced oscillation (PIO)

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APA (6th Edition):

Lee, B. P. (2012). Pilot and control system modelling for handling qualities analysis of large transport aircraft. (Doctoral Dissertation). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/10203

Chicago Manual of Style (16th Edition):

Lee, Brian P. “Pilot and control system modelling for handling qualities analysis of large transport aircraft.” 2012. Doctoral Dissertation, Cranfield University. Accessed January 25, 2021. http://dspace.lib.cranfield.ac.uk/handle/1826/10203.

MLA Handbook (7th Edition):

Lee, Brian P. “Pilot and control system modelling for handling qualities analysis of large transport aircraft.” 2012. Web. 25 Jan 2021.

Vancouver:

Lee BP. Pilot and control system modelling for handling qualities analysis of large transport aircraft. [Internet] [Doctoral dissertation]. Cranfield University; 2012. [cited 2021 Jan 25]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/10203.

Council of Science Editors:

Lee BP. Pilot and control system modelling for handling qualities analysis of large transport aircraft. [Doctoral Dissertation]. Cranfield University; 2012. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/10203


Cranfield University

2. Lee, Brian P. Pilot and control system modelling for handling qualities analysis of large transport aircraft.

Degree: PhD, 2012, Cranfield University

 The notion of airplane stability and control being a balancing act between stability and control has been around as long as aeronautics. The Wright brothers’… (more)

Subjects/Keywords: 629.13; Stability and control; Flight dynamics; Flying qualities; Pilot induced oscillation (PIO)

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Lee, B. P. (2012). Pilot and control system modelling for handling qualities analysis of large transport aircraft. (Doctoral Dissertation). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/10203 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.691002

Chicago Manual of Style (16th Edition):

Lee, Brian P. “Pilot and control system modelling for handling qualities analysis of large transport aircraft.” 2012. Doctoral Dissertation, Cranfield University. Accessed January 25, 2021. http://dspace.lib.cranfield.ac.uk/handle/1826/10203 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.691002.

MLA Handbook (7th Edition):

Lee, Brian P. “Pilot and control system modelling for handling qualities analysis of large transport aircraft.” 2012. Web. 25 Jan 2021.

Vancouver:

Lee BP. Pilot and control system modelling for handling qualities analysis of large transport aircraft. [Internet] [Doctoral dissertation]. Cranfield University; 2012. [cited 2021 Jan 25]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/10203 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.691002.

Council of Science Editors:

Lee BP. Pilot and control system modelling for handling qualities analysis of large transport aircraft. [Doctoral Dissertation]. Cranfield University; 2012. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/10203 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.691002

3. Liu, Qingling. Pilot-induced oscillation detection and mitigation.

Degree: MSc by Research, 2012, Cranfield University

 The aim of this thesis is to develop a real time PIO detection and mitigation system that consists of a detector based on short time… (more)

Subjects/Keywords: Pilot Vehicle System; Flight Control System; Pilot Induced Oscillation; Aircraft Pilot Coupling; Short Time Fourier Transform; ARX Model; Adaptive Controller; Pilot Modelling

…Loop Onset Point Primary Flight Display Proportional and Integral Pilot-Induced-Oscillation… …Pilot Vehicle System Real-Time Oscillation Verifier ROVER Integer Value Root Mean Squared… …Introduction Unintended aircraft pilot interactions that lead to unexpected oscillation motion in… …aircraft attitude and flight path are normally regarded as Pilot-induced oscillations, Pilot… …tendency for pilot-induced oscillations, that is, sustained or uncontrollable oscillations… 

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APA (6th Edition):

Liu, Q. (2012). Pilot-induced oscillation detection and mitigation. (Masters Thesis). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/7998

Chicago Manual of Style (16th Edition):

Liu, Qingling. “Pilot-induced oscillation detection and mitigation.” 2012. Masters Thesis, Cranfield University. Accessed January 25, 2021. http://dspace.lib.cranfield.ac.uk/handle/1826/7998.

MLA Handbook (7th Edition):

Liu, Qingling. “Pilot-induced oscillation detection and mitigation.” 2012. Web. 25 Jan 2021.

Vancouver:

Liu Q. Pilot-induced oscillation detection and mitigation. [Internet] [Masters thesis]. Cranfield University; 2012. [cited 2021 Jan 25]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/7998.

Council of Science Editors:

Liu Q. Pilot-induced oscillation detection and mitigation. [Masters Thesis]. Cranfield University; 2012. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/7998


University of Pretoria

4. [No author]. Longitudinal handling characteristics of a tailless gull-wing aircraft .

Degree: 2008, University of Pretoria

 A handling quality investigation was performed on the swept gull-wing configuration. The swept gull-wing configuration is tailless and has a wing with a transition in… (more)

Subjects/Keywords: Flight simulation; Tumbling; Thumbprint criterion; Neal-smith analysis; C-star criterion; Shomber-gertsen analysis; Pilot induced oscillation; Oswald efficiency; Pilot mathematical model; Variable sweep wing; Exulans; Variable static margin; Swept gull-wing configuration; O-point; E-point; Handling qualities; Gust handling qualities; Tailless aircraft; Pecking; Monnich and dalldorff criterion; UCTD

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APA (6th Edition):

author], [. (2008). Longitudinal handling characteristics of a tailless gull-wing aircraft . (Masters Thesis). University of Pretoria. Retrieved from http://upetd.up.ac.za/thesis/available/etd-09182008-132941/

Chicago Manual of Style (16th Edition):

author], [No. “Longitudinal handling characteristics of a tailless gull-wing aircraft .” 2008. Masters Thesis, University of Pretoria. Accessed January 25, 2021. http://upetd.up.ac.za/thesis/available/etd-09182008-132941/.

MLA Handbook (7th Edition):

author], [No. “Longitudinal handling characteristics of a tailless gull-wing aircraft .” 2008. Web. 25 Jan 2021.

Vancouver:

author] [. Longitudinal handling characteristics of a tailless gull-wing aircraft . [Internet] [Masters thesis]. University of Pretoria; 2008. [cited 2021 Jan 25]. Available from: http://upetd.up.ac.za/thesis/available/etd-09182008-132941/.

Council of Science Editors:

author] [. Longitudinal handling characteristics of a tailless gull-wing aircraft . [Masters Thesis]. University of Pretoria; 2008. Available from: http://upetd.up.ac.za/thesis/available/etd-09182008-132941/


University of Pretoria

5. Agenbag, Daniel Sarel. Longitudinal handling characteristics of a tailless gull-wing aircraft.

Degree: Mechanical and Aeronautical Engineering, 2008, University of Pretoria

 A handling quality investigation was performed on the swept gull-wing configuration. The swept gull-wing configuration is tailless and has a wing with a transition in… (more)

Subjects/Keywords: Flight simulation; Tumbling; Thumbprint criterion; Neal-smith analysis; C-star criterion; Shomber-gertsen analysis; Pilot induced oscillation; Oswald efficiency; Pilot mathematical model; Variable sweep wing; Exulans; Variable static margin; Swept gull-wing configuration; O-point; E-point; Handling qualities; Gust handling qualities; Tailless aircraft; Pecking; Monnich and dalldorff criterion; UCTD

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Agenbag, D. (2008). Longitudinal handling characteristics of a tailless gull-wing aircraft. (Masters Thesis). University of Pretoria. Retrieved from http://hdl.handle.net/2263/28011

Chicago Manual of Style (16th Edition):

Agenbag, Daniel. “Longitudinal handling characteristics of a tailless gull-wing aircraft.” 2008. Masters Thesis, University of Pretoria. Accessed January 25, 2021. http://hdl.handle.net/2263/28011.

MLA Handbook (7th Edition):

Agenbag, Daniel. “Longitudinal handling characteristics of a tailless gull-wing aircraft.” 2008. Web. 25 Jan 2021.

Vancouver:

Agenbag D. Longitudinal handling characteristics of a tailless gull-wing aircraft. [Internet] [Masters thesis]. University of Pretoria; 2008. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/2263/28011.

Council of Science Editors:

Agenbag D. Longitudinal handling characteristics of a tailless gull-wing aircraft. [Masters Thesis]. University of Pretoria; 2008. Available from: http://hdl.handle.net/2263/28011

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