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You searched for subject:(Flight simulation). Showing records 1 – 30 of 145 total matches.

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Addis Ababa University

1. Mathewos, Essatu. SIMULATION OF FLIGHT FOLLOWING SYSTEM .

Degree: 2012, Addis Ababa University

 The simulation of the flight following system i6 primarily chosen in the interest of Ethiopian Airlines need to implement the system to replace the currently… (more)

Subjects/Keywords: SIMULATION OF FLIGHT

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

APA (6th Edition):

Mathewos, E. (2012). SIMULATION OF FLIGHT FOLLOWING SYSTEM . (Thesis). Addis Ababa University. Retrieved from http://etd.aau.edu.et/dspace/handle/123456789/4410

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Mathewos, Essatu. “SIMULATION OF FLIGHT FOLLOWING SYSTEM .” 2012. Thesis, Addis Ababa University. Accessed January 18, 2021. http://etd.aau.edu.et/dspace/handle/123456789/4410.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Mathewos, Essatu. “SIMULATION OF FLIGHT FOLLOWING SYSTEM .” 2012. Web. 18 Jan 2021.

Vancouver:

Mathewos E. SIMULATION OF FLIGHT FOLLOWING SYSTEM . [Internet] [Thesis]. Addis Ababa University; 2012. [cited 2021 Jan 18]. Available from: http://etd.aau.edu.et/dspace/handle/123456789/4410.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Mathewos E. SIMULATION OF FLIGHT FOLLOWING SYSTEM . [Thesis]. Addis Ababa University; 2012. Available from: http://etd.aau.edu.et/dspace/handle/123456789/4410

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Uppsala University

2. Bylander, Ulf. Flight Path Simulation Application : A flight simulator for charged particle transport.

Degree: High Energy Physics, 2014, Uppsala University

  CTF3 is a test facility for a new CLIC high energy linear collider. For this beamsteering and beam focusing is vital. Because physically running… (more)

Subjects/Keywords: Simulation flight path

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APA (6th Edition):

Bylander, U. (2014). Flight Path Simulation Application : A flight simulator for charged particle transport. (Thesis). Uppsala University. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:uu:diva-227759

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Bylander, Ulf. “Flight Path Simulation Application : A flight simulator for charged particle transport.” 2014. Thesis, Uppsala University. Accessed January 18, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:uu:diva-227759.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Bylander, Ulf. “Flight Path Simulation Application : A flight simulator for charged particle transport.” 2014. Web. 18 Jan 2021.

Vancouver:

Bylander U. Flight Path Simulation Application : A flight simulator for charged particle transport. [Internet] [Thesis]. Uppsala University; 2014. [cited 2021 Jan 18]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:uu:diva-227759.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Bylander U. Flight Path Simulation Application : A flight simulator for charged particle transport. [Thesis]. Uppsala University; 2014. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:uu:diva-227759

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Uppsala University

3. Bylander, Ulf. Flight Path Simulation Application : A flight simulator for charged particle transport.

Degree: High Energy Physics, 2014, Uppsala University

CTF3 is a test facility for a new CLIC high energy linear collider. For this beamsteering and beam focusing is vital. Because physically running… (more)

Subjects/Keywords: Simulation flight path

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APA (6th Edition):

Bylander, U. (2014). Flight Path Simulation Application : A flight simulator for charged particle transport. (Thesis). Uppsala University. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:uu:diva-231090

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Bylander, Ulf. “Flight Path Simulation Application : A flight simulator for charged particle transport.” 2014. Thesis, Uppsala University. Accessed January 18, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:uu:diva-231090.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Bylander, Ulf. “Flight Path Simulation Application : A flight simulator for charged particle transport.” 2014. Web. 18 Jan 2021.

Vancouver:

Bylander U. Flight Path Simulation Application : A flight simulator for charged particle transport. [Internet] [Thesis]. Uppsala University; 2014. [cited 2021 Jan 18]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:uu:diva-231090.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Bylander U. Flight Path Simulation Application : A flight simulator for charged particle transport. [Thesis]. Uppsala University; 2014. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:uu:diva-231090

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Brunel University

4. Bromfield, Michael. Criteria for acceptable stick force gradients of a light aeroplane.

Degree: PhD, 2012, Brunel University

 During the period 1980 to 2008 there were 359 fatal accidents involving UK registered light aeroplanes of which 36% occurred in visual meteorological conditions. In… (more)

Subjects/Keywords: 363.12; Flight safety; Control feel; Pilot workload; Flight simulation; Flight test

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APA (6th Edition):

Bromfield, M. (2012). Criteria for acceptable stick force gradients of a light aeroplane. (Doctoral Dissertation). Brunel University. Retrieved from http://bura.brunel.ac.uk/handle/2438/6861 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.557870

Chicago Manual of Style (16th Edition):

Bromfield, Michael. “Criteria for acceptable stick force gradients of a light aeroplane.” 2012. Doctoral Dissertation, Brunel University. Accessed January 18, 2021. http://bura.brunel.ac.uk/handle/2438/6861 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.557870.

MLA Handbook (7th Edition):

Bromfield, Michael. “Criteria for acceptable stick force gradients of a light aeroplane.” 2012. Web. 18 Jan 2021.

Vancouver:

Bromfield M. Criteria for acceptable stick force gradients of a light aeroplane. [Internet] [Doctoral dissertation]. Brunel University; 2012. [cited 2021 Jan 18]. Available from: http://bura.brunel.ac.uk/handle/2438/6861 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.557870.

Council of Science Editors:

Bromfield M. Criteria for acceptable stick force gradients of a light aeroplane. [Doctoral Dissertation]. Brunel University; 2012. Available from: http://bura.brunel.ac.uk/handle/2438/6861 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.557870


Texas A&M University

5. Harris, Joshua A. Nonlinear Adaptive Dynamic Inversion Control for Variable Stability Small Unmanned Aircraft Systems.

Degree: MS, Aerospace Engineering, 2017, Texas A&M University

 In-flight simulation and variable stability aircraft provide useful capabilities for flight controls development such as testing control laws for new aircraft earlier, identification of adverse… (more)

Subjects/Keywords: adaptive control; dynamic inversion; flight control; in-flight simulation

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APA (6th Edition):

Harris, J. A. (2017). Nonlinear Adaptive Dynamic Inversion Control for Variable Stability Small Unmanned Aircraft Systems. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/169626

Chicago Manual of Style (16th Edition):

Harris, Joshua A. “Nonlinear Adaptive Dynamic Inversion Control for Variable Stability Small Unmanned Aircraft Systems.” 2017. Masters Thesis, Texas A&M University. Accessed January 18, 2021. http://hdl.handle.net/1969.1/169626.

MLA Handbook (7th Edition):

Harris, Joshua A. “Nonlinear Adaptive Dynamic Inversion Control for Variable Stability Small Unmanned Aircraft Systems.” 2017. Web. 18 Jan 2021.

Vancouver:

Harris JA. Nonlinear Adaptive Dynamic Inversion Control for Variable Stability Small Unmanned Aircraft Systems. [Internet] [Masters thesis]. Texas A&M University; 2017. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1969.1/169626.

Council of Science Editors:

Harris JA. Nonlinear Adaptive Dynamic Inversion Control for Variable Stability Small Unmanned Aircraft Systems. [Masters Thesis]. Texas A&M University; 2017. Available from: http://hdl.handle.net/1969.1/169626


Mississippi State University

6. Germann, Kenneth Paul. T-6A TEXAN II IN-FLIGHT SIMULATION AND VARIABLE STABILITY SYSTEM DESIGN.

Degree: PhD, Aerospace Engineering, 2009, Mississippi State University

 In-flight variable stability aircraft and in-flight simulation are described. The uses of these vehicles and the associated requirements are described. Several forms of control architecture… (more)

Subjects/Keywords: control; simulation; flight

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APA (6th Edition):

Germann, K. P. (2009). T-6A TEXAN II IN-FLIGHT SIMULATION AND VARIABLE STABILITY SYSTEM DESIGN. (Doctoral Dissertation). Mississippi State University. Retrieved from http://sun.library.msstate.edu/ETD-db/theses/available/etd-12162009-091123/ ;

Chicago Manual of Style (16th Edition):

Germann, Kenneth Paul. “T-6A TEXAN II IN-FLIGHT SIMULATION AND VARIABLE STABILITY SYSTEM DESIGN.” 2009. Doctoral Dissertation, Mississippi State University. Accessed January 18, 2021. http://sun.library.msstate.edu/ETD-db/theses/available/etd-12162009-091123/ ;.

MLA Handbook (7th Edition):

Germann, Kenneth Paul. “T-6A TEXAN II IN-FLIGHT SIMULATION AND VARIABLE STABILITY SYSTEM DESIGN.” 2009. Web. 18 Jan 2021.

Vancouver:

Germann KP. T-6A TEXAN II IN-FLIGHT SIMULATION AND VARIABLE STABILITY SYSTEM DESIGN. [Internet] [Doctoral dissertation]. Mississippi State University; 2009. [cited 2021 Jan 18]. Available from: http://sun.library.msstate.edu/ETD-db/theses/available/etd-12162009-091123/ ;.

Council of Science Editors:

Germann KP. T-6A TEXAN II IN-FLIGHT SIMULATION AND VARIABLE STABILITY SYSTEM DESIGN. [Doctoral Dissertation]. Mississippi State University; 2009. Available from: http://sun.library.msstate.edu/ETD-db/theses/available/etd-12162009-091123/ ;


McMaster University

7. Zeitoun, Omar. A Distributed System Interface for a Flight Simulator.

Degree: MASc, 2014, McMaster University

The importance of flight training has been realized since the inception of manned flight. In this thesis, a project about the interfacing of hardware cockpit… (more)

Subjects/Keywords: flight simulation; distributed system; interface; cessna 172

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APA (6th Edition):

Zeitoun, O. (2014). A Distributed System Interface for a Flight Simulator. (Masters Thesis). McMaster University. Retrieved from http://hdl.handle.net/11375/16298

Chicago Manual of Style (16th Edition):

Zeitoun, Omar. “A Distributed System Interface for a Flight Simulator.” 2014. Masters Thesis, McMaster University. Accessed January 18, 2021. http://hdl.handle.net/11375/16298.

MLA Handbook (7th Edition):

Zeitoun, Omar. “A Distributed System Interface for a Flight Simulator.” 2014. Web. 18 Jan 2021.

Vancouver:

Zeitoun O. A Distributed System Interface for a Flight Simulator. [Internet] [Masters thesis]. McMaster University; 2014. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/11375/16298.

Council of Science Editors:

Zeitoun O. A Distributed System Interface for a Flight Simulator. [Masters Thesis]. McMaster University; 2014. Available from: http://hdl.handle.net/11375/16298


University of Toronto

8. Khan, Jacek Filip. The Role of Internal Noise in Self-Motion Perception.

Degree: 2016, University of Toronto

In this study, vestibular-based motion perception was investigated. The vestibular system, located in the inner ear, is responsible for sensing translational and rotational motion. A… (more)

Subjects/Keywords: Flight Simulation; Motion Perception; Threshold; Vestibular; 0538

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APA (6th Edition):

Khan, J. F. (2016). The Role of Internal Noise in Self-Motion Perception. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/74961

Chicago Manual of Style (16th Edition):

Khan, Jacek Filip. “The Role of Internal Noise in Self-Motion Perception.” 2016. Masters Thesis, University of Toronto. Accessed January 18, 2021. http://hdl.handle.net/1807/74961.

MLA Handbook (7th Edition):

Khan, Jacek Filip. “The Role of Internal Noise in Self-Motion Perception.” 2016. Web. 18 Jan 2021.

Vancouver:

Khan JF. The Role of Internal Noise in Self-Motion Perception. [Internet] [Masters thesis]. University of Toronto; 2016. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1807/74961.

Council of Science Editors:

Khan JF. The Role of Internal Noise in Self-Motion Perception. [Masters Thesis]. University of Toronto; 2016. Available from: http://hdl.handle.net/1807/74961


Nanyang Technological University

9. Xie, Zhen. Forecasting, visibility and 3D route optimization for future air traffic management .

Degree: 2018, Nanyang Technological University

 Based on time-series Recurrent Neural Network (RNN) forecasting results, air traffic volumes and air passenger volumes will keep increasing for the coming decades. It will… (more)

Subjects/Keywords: DRNTU::Engineering::Aeronautical engineering::Flight simulation

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APA (6th Edition):

Xie, Z. (2018). Forecasting, visibility and 3D route optimization for future air traffic management . (Thesis). Nanyang Technological University. Retrieved from http://hdl.handle.net/10220/45896

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Xie, Zhen. “Forecasting, visibility and 3D route optimization for future air traffic management .” 2018. Thesis, Nanyang Technological University. Accessed January 18, 2021. http://hdl.handle.net/10220/45896.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Xie, Zhen. “Forecasting, visibility and 3D route optimization for future air traffic management .” 2018. Web. 18 Jan 2021.

Vancouver:

Xie Z. Forecasting, visibility and 3D route optimization for future air traffic management . [Internet] [Thesis]. Nanyang Technological University; 2018. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/10220/45896.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Xie Z. Forecasting, visibility and 3D route optimization for future air traffic management . [Thesis]. Nanyang Technological University; 2018. Available from: http://hdl.handle.net/10220/45896

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


University of Toronto

10. Abbasi, Humayoon. Simulation of Flexible Aircraft.

Degree: 2010, University of Toronto

This study aims to improve flight simulation of flexible aircraft. More specifically, this thesis concentrates on comparing two flexible aircraft flight simulation models. Both modeling… (more)

Subjects/Keywords: Simulation; Flexible; Deformable; Flight Dynamics; 0538

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APA (6th Edition):

Abbasi, H. (2010). Simulation of Flexible Aircraft. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/24523

Chicago Manual of Style (16th Edition):

Abbasi, Humayoon. “Simulation of Flexible Aircraft.” 2010. Masters Thesis, University of Toronto. Accessed January 18, 2021. http://hdl.handle.net/1807/24523.

MLA Handbook (7th Edition):

Abbasi, Humayoon. “Simulation of Flexible Aircraft.” 2010. Web. 18 Jan 2021.

Vancouver:

Abbasi H. Simulation of Flexible Aircraft. [Internet] [Masters thesis]. University of Toronto; 2010. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1807/24523.

Council of Science Editors:

Abbasi H. Simulation of Flexible Aircraft. [Masters Thesis]. University of Toronto; 2010. Available from: http://hdl.handle.net/1807/24523


University of Southern California

11. Kerci, Endri. The effect of Xᵤ and T_{theta_2} on autonomous in-flight refueling: a global Hawk RQ-4A approach.

Degree: MS, Aerospace Engineering, 2013, University of Southern California

 The effect of two parameters, Xᵤ and Ttheta2 , are explored for their influence on autonomous in-flight aerial refueling. It is believed that these two… (more)

Subjects/Keywords: autonomous; Global Hawk; in-flight refueling; simulation

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APA (6th Edition):

Kerci, E. (2013). The effect of Xᵤ and T_{theta_2} on autonomous in-flight refueling: a global Hawk RQ-4A approach. (Masters Thesis). University of Southern California. Retrieved from http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/306375/rec/6632

Chicago Manual of Style (16th Edition):

Kerci, Endri. “The effect of Xᵤ and T_{theta_2} on autonomous in-flight refueling: a global Hawk RQ-4A approach.” 2013. Masters Thesis, University of Southern California. Accessed January 18, 2021. http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/306375/rec/6632.

MLA Handbook (7th Edition):

Kerci, Endri. “The effect of Xᵤ and T_{theta_2} on autonomous in-flight refueling: a global Hawk RQ-4A approach.” 2013. Web. 18 Jan 2021.

Vancouver:

Kerci E. The effect of Xᵤ and T_{theta_2} on autonomous in-flight refueling: a global Hawk RQ-4A approach. [Internet] [Masters thesis]. University of Southern California; 2013. [cited 2021 Jan 18]. Available from: http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/306375/rec/6632.

Council of Science Editors:

Kerci E. The effect of Xᵤ and T_{theta_2} on autonomous in-flight refueling: a global Hawk RQ-4A approach. [Masters Thesis]. University of Southern California; 2013. Available from: http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/306375/rec/6632


Linköping University

12. Gustafsson, Anders. Use of head mounted virtual reality displays in flight training simulation.

Degree: Software and Systems, 2018, Linköping University

  The purpose of this thesis was to evaluate currently commercially available head mounted virtual reality displays for potential use in pilot training simulators. For… (more)

Subjects/Keywords: VR; Virtual reality; Flight simulation; Flight training simulation; Head mounted displays; HMD; Computer Engineering; Datorteknik

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APA (6th Edition):

Gustafsson, A. (2018). Use of head mounted virtual reality displays in flight training simulation. (Thesis). Linköping University. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-154016

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Gustafsson, Anders. “Use of head mounted virtual reality displays in flight training simulation.” 2018. Thesis, Linköping University. Accessed January 18, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-154016.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Gustafsson, Anders. “Use of head mounted virtual reality displays in flight training simulation.” 2018. Web. 18 Jan 2021.

Vancouver:

Gustafsson A. Use of head mounted virtual reality displays in flight training simulation. [Internet] [Thesis]. Linköping University; 2018. [cited 2021 Jan 18]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-154016.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Gustafsson A. Use of head mounted virtual reality displays in flight training simulation. [Thesis]. Linköping University; 2018. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-154016

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


University of Toronto

13. Ko, Shuk Fai (Eska). Investigation of Simulator Motion Drive Algorithms for Airplane Upset Simulation.

Degree: 2012, University of Toronto

Currently, it is uncertain how well a typical ground-based simulator's hexapod motion system can simulate the aggressive motion during airplane upset. To address this issue,… (more)

Subjects/Keywords: Motion Drive Algorithms; Flight Simulation; Airplane upset; Upset Recovery Simulation; 0538

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APA (6th Edition):

Ko, S. F. (. (2012). Investigation of Simulator Motion Drive Algorithms for Airplane Upset Simulation. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/35019

Chicago Manual of Style (16th Edition):

Ko, Shuk Fai (Eska). “Investigation of Simulator Motion Drive Algorithms for Airplane Upset Simulation.” 2012. Masters Thesis, University of Toronto. Accessed January 18, 2021. http://hdl.handle.net/1807/35019.

MLA Handbook (7th Edition):

Ko, Shuk Fai (Eska). “Investigation of Simulator Motion Drive Algorithms for Airplane Upset Simulation.” 2012. Web. 18 Jan 2021.

Vancouver:

Ko SF(. Investigation of Simulator Motion Drive Algorithms for Airplane Upset Simulation. [Internet] [Masters thesis]. University of Toronto; 2012. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1807/35019.

Council of Science Editors:

Ko SF(. Investigation of Simulator Motion Drive Algorithms for Airplane Upset Simulation. [Masters Thesis]. University of Toronto; 2012. Available from: http://hdl.handle.net/1807/35019

14. Ackerman, Kasey. Development of a pilot-in-the-loop flight simulator using NASA's transport class model.

Degree: MS, 0133, 2014, University of Illinois – Urbana-Champaign

 This thesis presents the development of an immersive flight simulator at the University of Illinois at Urbana-Champaign using NASA's Transport Class Model. Flight simulators are… (more)

Subjects/Keywords: flight simulation; simulation software

…architecture will require extensive software and PITL simulation prior to flight tests using a… …the need to develop a method for improving simulation performance during flight testing, and… …simulations, desktop flight simulation, or full-scale PITL testing without the need to implement the… …and flight control software tools are implemented. Depending on the simulation mode, the… …flight simulation and desktop piloted simulation, a pacer block provided by NASA is used in the… 

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APA (6th Edition):

Ackerman, K. (2014). Development of a pilot-in-the-loop flight simulator using NASA's transport class model. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/50650

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Ackerman, Kasey. “Development of a pilot-in-the-loop flight simulator using NASA's transport class model.” 2014. Thesis, University of Illinois – Urbana-Champaign. Accessed January 18, 2021. http://hdl.handle.net/2142/50650.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Ackerman, Kasey. “Development of a pilot-in-the-loop flight simulator using NASA's transport class model.” 2014. Web. 18 Jan 2021.

Vancouver:

Ackerman K. Development of a pilot-in-the-loop flight simulator using NASA's transport class model. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2014. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/2142/50650.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Ackerman K. Development of a pilot-in-the-loop flight simulator using NASA's transport class model. [Thesis]. University of Illinois – Urbana-Champaign; 2014. Available from: http://hdl.handle.net/2142/50650

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Cranfield University

15. Lone, M. Mudassir. Pilot modelling for airframe loads analysis.

Degree: PhD, 2013, Cranfield University

 The development of large lightweight airframes has resulted in what used to be high frequency structural dynamics entering the low frequency range associated with an… (more)

Subjects/Keywords: Pilot modelling; manual control; pilot-model-in-the-loop simulation; flight loads; aeroelastics; flight control

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APA (6th Edition):

Lone, M. M. (2013). Pilot modelling for airframe loads analysis. (Doctoral Dissertation). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/10388

Chicago Manual of Style (16th Edition):

Lone, M Mudassir. “Pilot modelling for airframe loads analysis.” 2013. Doctoral Dissertation, Cranfield University. Accessed January 18, 2021. http://dspace.lib.cranfield.ac.uk/handle/1826/10388.

MLA Handbook (7th Edition):

Lone, M Mudassir. “Pilot modelling for airframe loads analysis.” 2013. Web. 18 Jan 2021.

Vancouver:

Lone MM. Pilot modelling for airframe loads analysis. [Internet] [Doctoral dissertation]. Cranfield University; 2013. [cited 2021 Jan 18]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/10388.

Council of Science Editors:

Lone MM. Pilot modelling for airframe loads analysis. [Doctoral Dissertation]. Cranfield University; 2013. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/10388


University of Victoria

16. Klein-Miloslavich, Andreas. Modeling, simulation, hardware development, and testing of a lab-scale airborne wind energy system.

Degree: Department of Mechanical Engineering, 2020, University of Victoria

 Airborne Wind Energy Systems (AWES) harness the power of high-altitude winds using tethered planes or kites. Continuous and reliable operation requires that AWES become autonomous… (more)

Subjects/Keywords: Airborne Wind Energy; Flight model; Prototype development; Quadplane; Vertical take-off and landing; Autopilot; Open-source; Flight simulation; Flight test

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APA (6th Edition):

Klein-Miloslavich, A. (2020). Modeling, simulation, hardware development, and testing of a lab-scale airborne wind energy system. (Masters Thesis). University of Victoria. Retrieved from http://hdl.handle.net/1828/11508

Chicago Manual of Style (16th Edition):

Klein-Miloslavich, Andreas. “Modeling, simulation, hardware development, and testing of a lab-scale airborne wind energy system.” 2020. Masters Thesis, University of Victoria. Accessed January 18, 2021. http://hdl.handle.net/1828/11508.

MLA Handbook (7th Edition):

Klein-Miloslavich, Andreas. “Modeling, simulation, hardware development, and testing of a lab-scale airborne wind energy system.” 2020. Web. 18 Jan 2021.

Vancouver:

Klein-Miloslavich A. Modeling, simulation, hardware development, and testing of a lab-scale airborne wind energy system. [Internet] [Masters thesis]. University of Victoria; 2020. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1828/11508.

Council of Science Editors:

Klein-Miloslavich A. Modeling, simulation, hardware development, and testing of a lab-scale airborne wind energy system. [Masters Thesis]. University of Victoria; 2020. Available from: http://hdl.handle.net/1828/11508


Penn State University

17. Saetti, Umberto. Rotorcraft Flight Control Design with Alleviation of Unsteady Rotor Loads.

Degree: 2019, Penn State University

 The objective of this research effort is to develop rotorcraft flight control laws that minimize unsteady rotor loads by acting solely through the primary flight(more)

Subjects/Keywords: rotorcraft; flight controls; flight dynamics and control; flight dynamics; simulation; aerospace; aircraft; rotorcraft control; aircraft control; load alleviation; automatica flight control system; AFCS; control systems

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APA (6th Edition):

Saetti, U. (2019). Rotorcraft Flight Control Design with Alleviation of Unsteady Rotor Loads. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/16696uxs116

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Saetti, Umberto. “Rotorcraft Flight Control Design with Alleviation of Unsteady Rotor Loads.” 2019. Thesis, Penn State University. Accessed January 18, 2021. https://submit-etda.libraries.psu.edu/catalog/16696uxs116.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Saetti, Umberto. “Rotorcraft Flight Control Design with Alleviation of Unsteady Rotor Loads.” 2019. Web. 18 Jan 2021.

Vancouver:

Saetti U. Rotorcraft Flight Control Design with Alleviation of Unsteady Rotor Loads. [Internet] [Thesis]. Penn State University; 2019. [cited 2021 Jan 18]. Available from: https://submit-etda.libraries.psu.edu/catalog/16696uxs116.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Saetti U. Rotorcraft Flight Control Design with Alleviation of Unsteady Rotor Loads. [Thesis]. Penn State University; 2019. Available from: https://submit-etda.libraries.psu.edu/catalog/16696uxs116

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

18. Reweti, Savern. PC-based aviation training devices for pilot training in visual flight rules procedures : development, validation and effectiveness.

Degree: PhD, Aviation, 2014, Massey University

 Flying is a difficult and complex activity that requires a significant level of attention from the pilot as well as a lengthy training period to… (more)

Subjects/Keywords: Flight simulators; Flight simulation; Aeroplanes; Piloting; Computer simulation; Flight training

…29 2.5 ....The Effect of Fidelity on Flight Simulation… …49 2.8.2 ...... Using PCATDs with Microsoft Flight Simulator… …50 2.8.3 ...... Using PCATDs for Instrument Flight Rules Training… …58 2.8.6 ...... Using PCATDs for Visual Flight Rules Training… …72 vi Chapter 3. Flight Training In New Zealand… 

Page 1 Page 2 Page 3 Page 4 Page 5 Page 6 Page 7

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APA (6th Edition):

Reweti, S. (2014). PC-based aviation training devices for pilot training in visual flight rules procedures : development, validation and effectiveness. (Doctoral Dissertation). Massey University. Retrieved from http://hdl.handle.net/10179/5454

Chicago Manual of Style (16th Edition):

Reweti, Savern. “PC-based aviation training devices for pilot training in visual flight rules procedures : development, validation and effectiveness.” 2014. Doctoral Dissertation, Massey University. Accessed January 18, 2021. http://hdl.handle.net/10179/5454.

MLA Handbook (7th Edition):

Reweti, Savern. “PC-based aviation training devices for pilot training in visual flight rules procedures : development, validation and effectiveness.” 2014. Web. 18 Jan 2021.

Vancouver:

Reweti S. PC-based aviation training devices for pilot training in visual flight rules procedures : development, validation and effectiveness. [Internet] [Doctoral dissertation]. Massey University; 2014. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/10179/5454.

Council of Science Editors:

Reweti S. PC-based aviation training devices for pilot training in visual flight rules procedures : development, validation and effectiveness. [Doctoral Dissertation]. Massey University; 2014. Available from: http://hdl.handle.net/10179/5454


Rochester Institute of Technology

19. Komendat, Andrew. Center-of-gravity estimation of an aircraft solely using traditional aircraft measurement sensors.

Degree: Mechanical Engineering, 2012, Rochester Institute of Technology

 In this work, a novel algorithm for estimating aircraft center-of-gravity location based solely on traditional aircraft measurements is investigated. The algorithm uses known physics-based kinematic… (more)

Subjects/Keywords: Aircraft; Center of gravity; Estimation; Flight dynamics; Optimization; Simulation

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APA (6th Edition):

Komendat, A. (2012). Center-of-gravity estimation of an aircraft solely using traditional aircraft measurement sensors. (Thesis). Rochester Institute of Technology. Retrieved from https://scholarworks.rit.edu/theses/195

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Komendat, Andrew. “Center-of-gravity estimation of an aircraft solely using traditional aircraft measurement sensors.” 2012. Thesis, Rochester Institute of Technology. Accessed January 18, 2021. https://scholarworks.rit.edu/theses/195.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Komendat, Andrew. “Center-of-gravity estimation of an aircraft solely using traditional aircraft measurement sensors.” 2012. Web. 18 Jan 2021.

Vancouver:

Komendat A. Center-of-gravity estimation of an aircraft solely using traditional aircraft measurement sensors. [Internet] [Thesis]. Rochester Institute of Technology; 2012. [cited 2021 Jan 18]. Available from: https://scholarworks.rit.edu/theses/195.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Komendat A. Center-of-gravity estimation of an aircraft solely using traditional aircraft measurement sensors. [Thesis]. Rochester Institute of Technology; 2012. Available from: https://scholarworks.rit.edu/theses/195

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


University of Michigan

20. Sharma, Abhinav. Development and Application of a Comprehensive Simulation for Modeling Helicopter Ship Landing.

Degree: PhD, Aerospace Engineering, 2019, University of Michigan

 This work presents a comprehensive first principles physics-based simulation capability for helicopter ship landing, denoted as "HeliUM2-umich." The simulation incorporates key components of the ship-helicopter… (more)

Subjects/Keywords: helicopter ship landing; modeling and simulation; flight dynamics; Aerospace Engineering; Engineering

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APA (6th Edition):

Sharma, A. (2019). Development and Application of a Comprehensive Simulation for Modeling Helicopter Ship Landing. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/153342

Chicago Manual of Style (16th Edition):

Sharma, Abhinav. “Development and Application of a Comprehensive Simulation for Modeling Helicopter Ship Landing.” 2019. Doctoral Dissertation, University of Michigan. Accessed January 18, 2021. http://hdl.handle.net/2027.42/153342.

MLA Handbook (7th Edition):

Sharma, Abhinav. “Development and Application of a Comprehensive Simulation for Modeling Helicopter Ship Landing.” 2019. Web. 18 Jan 2021.

Vancouver:

Sharma A. Development and Application of a Comprehensive Simulation for Modeling Helicopter Ship Landing. [Internet] [Doctoral dissertation]. University of Michigan; 2019. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/2027.42/153342.

Council of Science Editors:

Sharma A. Development and Application of a Comprehensive Simulation for Modeling Helicopter Ship Landing. [Doctoral Dissertation]. University of Michigan; 2019. Available from: http://hdl.handle.net/2027.42/153342


University of Toronto

21. Peterson, Timothy Shaw. Handling Qualities of a Blended Wing Body Aircraft.

Degree: 2011, University of Toronto

The blended wing body (BWB) is a tailless aircraft with the potential to use 27% less fuel than a conventional aircraft with the same passenger… (more)

Subjects/Keywords: flight simulation; handling qualities; blended wing body; 0538

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APA (6th Edition):

Peterson, T. S. (2011). Handling Qualities of a Blended Wing Body Aircraft. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/31384

Chicago Manual of Style (16th Edition):

Peterson, Timothy Shaw. “Handling Qualities of a Blended Wing Body Aircraft.” 2011. Masters Thesis, University of Toronto. Accessed January 18, 2021. http://hdl.handle.net/1807/31384.

MLA Handbook (7th Edition):

Peterson, Timothy Shaw. “Handling Qualities of a Blended Wing Body Aircraft.” 2011. Web. 18 Jan 2021.

Vancouver:

Peterson TS. Handling Qualities of a Blended Wing Body Aircraft. [Internet] [Masters thesis]. University of Toronto; 2011. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1807/31384.

Council of Science Editors:

Peterson TS. Handling Qualities of a Blended Wing Body Aircraft. [Masters Thesis]. University of Toronto; 2011. Available from: http://hdl.handle.net/1807/31384


Delft University of Technology

22. Martín Fernández, Patricia A (author). Impact of Integrated RPAS Operations in TMA.

Degree: 2019, Delft University of Technology

The fastgrowing Unmanned Aircraft scene accounts for an increasing number of new users who should have access to the airspace as any other full-fledged airspace… (more)

Subjects/Keywords: RPAS; UAS; ATM; UTM; Flight Performance; Fast-time simulation

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APA (6th Edition):

Martín Fernández, P. A. (. (2019). Impact of Integrated RPAS Operations in TMA. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:337957d0-1bd2-4d0b-9b36-725636d52826

Chicago Manual of Style (16th Edition):

Martín Fernández, Patricia A (author). “Impact of Integrated RPAS Operations in TMA.” 2019. Masters Thesis, Delft University of Technology. Accessed January 18, 2021. http://resolver.tudelft.nl/uuid:337957d0-1bd2-4d0b-9b36-725636d52826.

MLA Handbook (7th Edition):

Martín Fernández, Patricia A (author). “Impact of Integrated RPAS Operations in TMA.” 2019. Web. 18 Jan 2021.

Vancouver:

Martín Fernández PA(. Impact of Integrated RPAS Operations in TMA. [Internet] [Masters thesis]. Delft University of Technology; 2019. [cited 2021 Jan 18]. Available from: http://resolver.tudelft.nl/uuid:337957d0-1bd2-4d0b-9b36-725636d52826.

Council of Science Editors:

Martín Fernández PA(. Impact of Integrated RPAS Operations in TMA. [Masters Thesis]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:337957d0-1bd2-4d0b-9b36-725636d52826


Nanyang Technological University

23. Adnan Maqsood. Longitudinal dynamics, optimization and control of aircraft transition maneuver using aerodynamic vectoring .

Degree: 2012, Nanyang Technological University

 In order to enhance the flight envelope of Unmanned Air Vehicles (UAVs), there have been efforts to combine the excellent hover capabilities of rotorcraft with… (more)

Subjects/Keywords: DRNTU::Engineering::Aeronautical engineering::Aircraft; DRNTU::Engineering::Aeronautical engineering::Flight simulation

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APA (6th Edition):

Maqsood, A. (2012). Longitudinal dynamics, optimization and control of aircraft transition maneuver using aerodynamic vectoring . (Thesis). Nanyang Technological University. Retrieved from http://hdl.handle.net/10356/48041

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Maqsood, Adnan. “Longitudinal dynamics, optimization and control of aircraft transition maneuver using aerodynamic vectoring .” 2012. Thesis, Nanyang Technological University. Accessed January 18, 2021. http://hdl.handle.net/10356/48041.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Maqsood, Adnan. “Longitudinal dynamics, optimization and control of aircraft transition maneuver using aerodynamic vectoring .” 2012. Web. 18 Jan 2021.

Vancouver:

Maqsood A. Longitudinal dynamics, optimization and control of aircraft transition maneuver using aerodynamic vectoring . [Internet] [Thesis]. Nanyang Technological University; 2012. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/10356/48041.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Maqsood A. Longitudinal dynamics, optimization and control of aircraft transition maneuver using aerodynamic vectoring . [Thesis]. Nanyang Technological University; 2012. Available from: http://hdl.handle.net/10356/48041

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

24. Yogeshwaran Jayaraman. Dynamics models of flexible aircraft .

Degree: 2014, Nanyang Technological University

 Recent trends in aircraft design owing to requirements of high performance and weight reduction have resulted in aircraft possessing significant structural flexibility. Under these conditions,… (more)

Subjects/Keywords: DRNTU::Engineering::Aeronautical engineering::Flight simulation; DRNTU::Engineering::Aeronautical engineering::Aircraft

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APA (6th Edition):

Jayaraman, Y. (2014). Dynamics models of flexible aircraft . (Thesis). Nanyang Technological University. Retrieved from http://hdl.handle.net/10356/61444

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Jayaraman, Yogeshwaran. “Dynamics models of flexible aircraft .” 2014. Thesis, Nanyang Technological University. Accessed January 18, 2021. http://hdl.handle.net/10356/61444.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Jayaraman, Yogeshwaran. “Dynamics models of flexible aircraft .” 2014. Web. 18 Jan 2021.

Vancouver:

Jayaraman Y. Dynamics models of flexible aircraft . [Internet] [Thesis]. Nanyang Technological University; 2014. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/10356/61444.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Jayaraman Y. Dynamics models of flexible aircraft . [Thesis]. Nanyang Technological University; 2014. Available from: http://hdl.handle.net/10356/61444

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


University of Toronto

25. Tse, Bosco Chun Bun. Effects of Inertial and Geometric Nonlinearities in the Simulation of Flexible Aircraft Dynamics.

Degree: 2013, University of Toronto

This thesis examines the relative importance of the inertial and geometric nonlinearities in modelling the dynamics of a flexible aircraft. Inertial nonlinearities are derived by… (more)

Subjects/Keywords: Flight Simulation; Flexible Aircraft; Geometric Nonlinearities; Inertial Nonlinearities; 0538

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APA (6th Edition):

Tse, B. C. B. (2013). Effects of Inertial and Geometric Nonlinearities in the Simulation of Flexible Aircraft Dynamics. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/42961

Chicago Manual of Style (16th Edition):

Tse, Bosco Chun Bun. “Effects of Inertial and Geometric Nonlinearities in the Simulation of Flexible Aircraft Dynamics.” 2013. Masters Thesis, University of Toronto. Accessed January 18, 2021. http://hdl.handle.net/1807/42961.

MLA Handbook (7th Edition):

Tse, Bosco Chun Bun. “Effects of Inertial and Geometric Nonlinearities in the Simulation of Flexible Aircraft Dynamics.” 2013. Web. 18 Jan 2021.

Vancouver:

Tse BCB. Effects of Inertial and Geometric Nonlinearities in the Simulation of Flexible Aircraft Dynamics. [Internet] [Masters thesis]. University of Toronto; 2013. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1807/42961.

Council of Science Editors:

Tse BCB. Effects of Inertial and Geometric Nonlinearities in the Simulation of Flexible Aircraft Dynamics. [Masters Thesis]. University of Toronto; 2013. Available from: http://hdl.handle.net/1807/42961


University of Manchester

26. Parslew, Ben. Simulating avian wingbeats and wakes.

Degree: PhD, 2012, University of Manchester

 Analytical models of avian flight have previously been used to predict mechanical and metabolic power consumption during cruise. These models are limited, in that they… (more)

Subjects/Keywords: 598; Avian; Predictive simulation; Flapping; Wake; Bird flight; Inverse dynamics

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APA (6th Edition):

Parslew, B. (2012). Simulating avian wingbeats and wakes. (Doctoral Dissertation). University of Manchester. Retrieved from https://www.research.manchester.ac.uk/portal/en/theses/simulating-avian-wingbeats-and-wakes(038035c2-fe9e-4104-92dc-544579c7011b).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.553489

Chicago Manual of Style (16th Edition):

Parslew, Ben. “Simulating avian wingbeats and wakes.” 2012. Doctoral Dissertation, University of Manchester. Accessed January 18, 2021. https://www.research.manchester.ac.uk/portal/en/theses/simulating-avian-wingbeats-and-wakes(038035c2-fe9e-4104-92dc-544579c7011b).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.553489.

MLA Handbook (7th Edition):

Parslew, Ben. “Simulating avian wingbeats and wakes.” 2012. Web. 18 Jan 2021.

Vancouver:

Parslew B. Simulating avian wingbeats and wakes. [Internet] [Doctoral dissertation]. University of Manchester; 2012. [cited 2021 Jan 18]. Available from: https://www.research.manchester.ac.uk/portal/en/theses/simulating-avian-wingbeats-and-wakes(038035c2-fe9e-4104-92dc-544579c7011b).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.553489.

Council of Science Editors:

Parslew B. Simulating avian wingbeats and wakes. [Doctoral Dissertation]. University of Manchester; 2012. Available from: https://www.research.manchester.ac.uk/portal/en/theses/simulating-avian-wingbeats-and-wakes(038035c2-fe9e-4104-92dc-544579c7011b).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.553489


Brno University of Technology

27. Sztefek, Jan. Model chování dynamických systémů: Model of Properties of Dynamic Systems.

Degree: 2019, Brno University of Technology

 The thesis deals with modeling algorithm for mathematical description of dynamical system written in status description, which makes it possible to changing coefficients status array… (more)

Subjects/Keywords: MatLab; Simulink; Dynamické systémy; MatLab; Simulink; Dynamic systems; plains flight simulation

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APA (6th Edition):

Sztefek, J. (2019). Model chování dynamických systémů: Model of Properties of Dynamic Systems. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/26499

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Sztefek, Jan. “Model chování dynamických systémů: Model of Properties of Dynamic Systems.” 2019. Thesis, Brno University of Technology. Accessed January 18, 2021. http://hdl.handle.net/11012/26499.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Sztefek, Jan. “Model chování dynamických systémů: Model of Properties of Dynamic Systems.” 2019. Web. 18 Jan 2021.

Vancouver:

Sztefek J. Model chování dynamických systémů: Model of Properties of Dynamic Systems. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/11012/26499.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Sztefek J. Model chování dynamických systémů: Model of Properties of Dynamic Systems. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/26499

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


University of Toronto

28. Leung, Jordan. Parameter Estimation Methods for High Angle-of-attack Aerodynamic Modelling.

Degree: 2019, University of Toronto

In recent years, extensive research has been performed in post-stall aerodynamic model development to facilitate the use of simulator-based stall recovery training for commercial pilots.… (more)

Subjects/Keywords: Aerodynamics; Dynamic Modelling; Flight Simulation; Parameter Estimation; Stall; System Identification; 0538

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APA (6th Edition):

Leung, J. (2019). Parameter Estimation Methods for High Angle-of-attack Aerodynamic Modelling. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/102971

Chicago Manual of Style (16th Edition):

Leung, Jordan. “Parameter Estimation Methods for High Angle-of-attack Aerodynamic Modelling.” 2019. Masters Thesis, University of Toronto. Accessed January 18, 2021. http://hdl.handle.net/1807/102971.

MLA Handbook (7th Edition):

Leung, Jordan. “Parameter Estimation Methods for High Angle-of-attack Aerodynamic Modelling.” 2019. Web. 18 Jan 2021.

Vancouver:

Leung J. Parameter Estimation Methods for High Angle-of-attack Aerodynamic Modelling. [Internet] [Masters thesis]. University of Toronto; 2019. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1807/102971.

Council of Science Editors:

Leung J. Parameter Estimation Methods for High Angle-of-attack Aerodynamic Modelling. [Masters Thesis]. University of Toronto; 2019. Available from: http://hdl.handle.net/1807/102971


Reykjavík University

29. Margrét Jóna Gestsdóttir 1988-. Agent based simulation of passenger demand for domestic air transport in Iceland .

Degree: 2016, Reykjavík University

 Reykjavík, the capital city of Iceland, has an airport located in the city centre. The central location of the airport has been debated for decades.… (more)

Subjects/Keywords: Rekstrarverkfræði; Meistaraprófsritgerðir; Hermilíkön; Innanlandsflug; Engineering management; Simulation; Flight

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APA (6th Edition):

1988-, M. J. G. (2016). Agent based simulation of passenger demand for domestic air transport in Iceland . (Thesis). Reykjavík University. Retrieved from http://hdl.handle.net/1946/23798

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

1988-, Margrét Jóna Gestsdóttir. “Agent based simulation of passenger demand for domestic air transport in Iceland .” 2016. Thesis, Reykjavík University. Accessed January 18, 2021. http://hdl.handle.net/1946/23798.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

1988-, Margrét Jóna Gestsdóttir. “Agent based simulation of passenger demand for domestic air transport in Iceland .” 2016. Web. 18 Jan 2021.

Vancouver:

1988- MJG. Agent based simulation of passenger demand for domestic air transport in Iceland . [Internet] [Thesis]. Reykjavík University; 2016. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1946/23798.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

1988- MJG. Agent based simulation of passenger demand for domestic air transport in Iceland . [Thesis]. Reykjavík University; 2016. Available from: http://hdl.handle.net/1946/23798

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Louisiana State University

30. Xia, Kai. Molecular Dynamics Simulation Study of Single DNA Nucleotides Transport Through Nanoslits.

Degree: PhD, Mechanical Engineering, 2015, Louisiana State University

 There is potential for flight time based DNA sequencing involving disassembly into individual nucleotides which would pass through a nanochannel with 2 or more detectors.… (more)

Subjects/Keywords: time of flight; DNA sequencing; molecular dynamics simulation; adsorption; ion association

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APA (6th Edition):

Xia, K. (2015). Molecular Dynamics Simulation Study of Single DNA Nucleotides Transport Through Nanoslits. (Doctoral Dissertation). Louisiana State University. Retrieved from etd-06222015-135811 ; https://digitalcommons.lsu.edu/gradschool_dissertations/2852

Chicago Manual of Style (16th Edition):

Xia, Kai. “Molecular Dynamics Simulation Study of Single DNA Nucleotides Transport Through Nanoslits.” 2015. Doctoral Dissertation, Louisiana State University. Accessed January 18, 2021. etd-06222015-135811 ; https://digitalcommons.lsu.edu/gradschool_dissertations/2852.

MLA Handbook (7th Edition):

Xia, Kai. “Molecular Dynamics Simulation Study of Single DNA Nucleotides Transport Through Nanoslits.” 2015. Web. 18 Jan 2021.

Vancouver:

Xia K. Molecular Dynamics Simulation Study of Single DNA Nucleotides Transport Through Nanoslits. [Internet] [Doctoral dissertation]. Louisiana State University; 2015. [cited 2021 Jan 18]. Available from: etd-06222015-135811 ; https://digitalcommons.lsu.edu/gradschool_dissertations/2852.

Council of Science Editors:

Xia K. Molecular Dynamics Simulation Study of Single DNA Nucleotides Transport Through Nanoslits. [Doctoral Dissertation]. Louisiana State University; 2015. Available from: etd-06222015-135811 ; https://digitalcommons.lsu.edu/gradschool_dissertations/2852

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