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You searched for subject:( aircraft). Showing records 1 – 30 of 2073 total matches.

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1. Belisle, Michael Joseph. Aerodynamic Design for Swept-wing Laminar Flow.

Degree: 2013, Texas Digital Library

 This work describes and compares processes for swept-wing laminar flow control (SWLFC) aerody-namic design. It focuses on results obtained during the preliminary outer-mold-line (OML) design… (more)

Subjects/Keywords: aircraft

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APA (6th Edition):

Belisle, M. J. (2013). Aerodynamic Design for Swept-wing Laminar Flow. (Thesis). Texas Digital Library. Retrieved from http://hdl.handle.net/1969; http://hdl.handle.net/2249.1/66548

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):

Belisle, Michael Joseph. “Aerodynamic Design for Swept-wing Laminar Flow.” 2013. Thesis, Texas Digital Library. Accessed March 31, 2020. http://hdl.handle.net/1969; http://hdl.handle.net/2249.1/66548.

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

MLA Handbook (7th Edition):

Belisle, Michael Joseph. “Aerodynamic Design for Swept-wing Laminar Flow.” 2013. Web. 31 Mar 2020.

Vancouver:

Belisle MJ. Aerodynamic Design for Swept-wing Laminar Flow. [Internet] [Thesis]. Texas Digital Library; 2013. [cited 2020 Mar 31]. Available from: http://hdl.handle.net/1969; http://hdl.handle.net/2249.1/66548.

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

Council of Science Editors:

Belisle MJ. Aerodynamic Design for Swept-wing Laminar Flow. [Thesis]. Texas Digital Library; 2013. Available from: http://hdl.handle.net/1969; http://hdl.handle.net/2249.1/66548

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


University of Nairobi

2. Tollo, Godfrey A. Aircraft maintenance support system for a commonly used engine type .

Degree: 2009, University of Nairobi

Aircraft fault isolation is an important function in aircraft maintenance. This project seeks to break new grounds in automation of this domain. AMSS is a… (more)

Subjects/Keywords: Aircraft maintenance; Aircraft Maintenance System

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APA (6th Edition):

Tollo, G. A. (2009). Aircraft maintenance support system for a commonly used engine type . (Thesis). University of Nairobi. Retrieved from http://erepository.uonbi.ac.ke:8080/xmlui/handle/123456789/20408

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):

Tollo, Godfrey A. “Aircraft maintenance support system for a commonly used engine type .” 2009. Thesis, University of Nairobi. Accessed March 31, 2020. http://erepository.uonbi.ac.ke:8080/xmlui/handle/123456789/20408.

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

MLA Handbook (7th Edition):

Tollo, Godfrey A. “Aircraft maintenance support system for a commonly used engine type .” 2009. Web. 31 Mar 2020.

Vancouver:

Tollo GA. Aircraft maintenance support system for a commonly used engine type . [Internet] [Thesis]. University of Nairobi; 2009. [cited 2020 Mar 31]. Available from: http://erepository.uonbi.ac.ke:8080/xmlui/handle/123456789/20408.

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

Council of Science Editors:

Tollo GA. Aircraft maintenance support system for a commonly used engine type . [Thesis]. University of Nairobi; 2009. Available from: http://erepository.uonbi.ac.ke:8080/xmlui/handle/123456789/20408

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


Stellenbosch University

3. Maneschijn, Anton. A framework and criteria for the operability of unmanned aircraft systems.

Degree: Electrical and Electronic Engineering, 2010, Stellenbosch University

Thesis (PhD (Electrical and Electronic Engineering)) – University of Stellenbosch, 2010.

Dissertation presented in fulfilment of the requirements for the degree of Doctor of Philosophy in… (more)

Subjects/Keywords: Unmanned aircraft; Aircraft; Operability; Airworthiness

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APA (6th Edition):

Maneschijn, A. (2010). A framework and criteria for the operability of unmanned aircraft systems. (Thesis). Stellenbosch University. Retrieved from http://hdl.handle.net/10019.1/5153

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):

Maneschijn, Anton. “A framework and criteria for the operability of unmanned aircraft systems.” 2010. Thesis, Stellenbosch University. Accessed March 31, 2020. http://hdl.handle.net/10019.1/5153.

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

MLA Handbook (7th Edition):

Maneschijn, Anton. “A framework and criteria for the operability of unmanned aircraft systems.” 2010. Web. 31 Mar 2020.

Vancouver:

Maneschijn A. A framework and criteria for the operability of unmanned aircraft systems. [Internet] [Thesis]. Stellenbosch University; 2010. [cited 2020 Mar 31]. Available from: http://hdl.handle.net/10019.1/5153.

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

Council of Science Editors:

Maneschijn A. A framework and criteria for the operability of unmanned aircraft systems. [Thesis]. Stellenbosch University; 2010. Available from: http://hdl.handle.net/10019.1/5153

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


Purdue University

4. Brewer, Cory Ryan. Techniques to Complete an Aircraft Appraisal.

Degree: MS, Aviation and Aerospace Management, 2013, Purdue University

  The industry of buying and selling aircraft has experienced financial volatility in demand and supply, but the current industry trends show major gains and… (more)

Subjects/Keywords: Aircraft Appraisal; Aircraft Leasing; Transportation

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APA (6th Edition):

Brewer, C. R. (2013). Techniques to Complete an Aircraft Appraisal. (Thesis). Purdue University. Retrieved from https://docs.lib.purdue.edu/open_access_theses/10

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):

Brewer, Cory Ryan. “Techniques to Complete an Aircraft Appraisal.” 2013. Thesis, Purdue University. Accessed March 31, 2020. https://docs.lib.purdue.edu/open_access_theses/10.

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

MLA Handbook (7th Edition):

Brewer, Cory Ryan. “Techniques to Complete an Aircraft Appraisal.” 2013. Web. 31 Mar 2020.

Vancouver:

Brewer CR. Techniques to Complete an Aircraft Appraisal. [Internet] [Thesis]. Purdue University; 2013. [cited 2020 Mar 31]. Available from: https://docs.lib.purdue.edu/open_access_theses/10.

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

Council of Science Editors:

Brewer CR. Techniques to Complete an Aircraft Appraisal. [Thesis]. Purdue University; 2013. Available from: https://docs.lib.purdue.edu/open_access_theses/10

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


California State University – Chico

5. Ghonsalves, Wilfred L. A Multi-Input Multi-Output Self Tuning Regulator for Nonlinear High Performance Aircraft Control .

Degree: 2010, California State University – Chico

 ABSTRACT A MULTI-INPUT MULTI-OUTPUT SELF TUNING REGULATOR FOR NONLINEAR HIGH PERFORMANCE AIRCRAFT CONTROL by Wilfred L. Ghonsalves Master of Science in Electrical and Computer Engineering… (more)

Subjects/Keywords: Aircraft Control

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APA (6th Edition):

Ghonsalves, W. L. (2010). A Multi-Input Multi-Output Self Tuning Regulator for Nonlinear High Performance Aircraft Control . (Thesis). California State University – Chico. Retrieved from http://hdl.handle.net/10211.4/237

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):

Ghonsalves, Wilfred L. “A Multi-Input Multi-Output Self Tuning Regulator for Nonlinear High Performance Aircraft Control .” 2010. Thesis, California State University – Chico. Accessed March 31, 2020. http://hdl.handle.net/10211.4/237.

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

MLA Handbook (7th Edition):

Ghonsalves, Wilfred L. “A Multi-Input Multi-Output Self Tuning Regulator for Nonlinear High Performance Aircraft Control .” 2010. Web. 31 Mar 2020.

Vancouver:

Ghonsalves WL. A Multi-Input Multi-Output Self Tuning Regulator for Nonlinear High Performance Aircraft Control . [Internet] [Thesis]. California State University – Chico; 2010. [cited 2020 Mar 31]. Available from: http://hdl.handle.net/10211.4/237.

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

Council of Science Editors:

Ghonsalves WL. A Multi-Input Multi-Output Self Tuning Regulator for Nonlinear High Performance Aircraft Control . [Thesis]. California State University – Chico; 2010. Available from: http://hdl.handle.net/10211.4/237

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


Oregon State University

6. Skeele, Ryan. Planning Under Uncertainty for Unmanned Aerial Vehicles.

Degree: MS, Robotics, 2016, Oregon State University

 Unmanned aerial vehicle (UAV) technology has grown out of traditional research and military applications and has captivated the commercial and consumer markets, showing the ability… (more)

Subjects/Keywords: Planning; Drone aircraft

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APA (6th Edition):

Skeele, R. (2016). Planning Under Uncertainty for Unmanned Aerial Vehicles. (Masters Thesis). Oregon State University. Retrieved from http://hdl.handle.net/1957/59456

Chicago Manual of Style (16th Edition):

Skeele, Ryan. “Planning Under Uncertainty for Unmanned Aerial Vehicles.” 2016. Masters Thesis, Oregon State University. Accessed March 31, 2020. http://hdl.handle.net/1957/59456.

MLA Handbook (7th Edition):

Skeele, Ryan. “Planning Under Uncertainty for Unmanned Aerial Vehicles.” 2016. Web. 31 Mar 2020.

Vancouver:

Skeele R. Planning Under Uncertainty for Unmanned Aerial Vehicles. [Internet] [Masters thesis]. Oregon State University; 2016. [cited 2020 Mar 31]. Available from: http://hdl.handle.net/1957/59456.

Council of Science Editors:

Skeele R. Planning Under Uncertainty for Unmanned Aerial Vehicles. [Masters Thesis]. Oregon State University; 2016. Available from: http://hdl.handle.net/1957/59456


University of Victoria

7. Rocha, Bruno Filipe Ferreira Graca. Structural health monitoring of aircraft structures: development of a phased array system.

Degree: Dept. of Mechanical Engineering, 2011, University of Victoria

 This work consisted in the research and development of a phased array embedded system for Structural Health Monitoring (SHM) of aircraft structures. This system is… (more)

Subjects/Keywords: airframes; aircraft structures

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APA (6th Edition):

Rocha, B. F. F. G. (2011). Structural health monitoring of aircraft structures: development of a phased array system. (Masters Thesis). University of Victoria. Retrieved from http://hdl.handle.net/1828/3604

Chicago Manual of Style (16th Edition):

Rocha, Bruno Filipe Ferreira Graca. “Structural health monitoring of aircraft structures: development of a phased array system.” 2011. Masters Thesis, University of Victoria. Accessed March 31, 2020. http://hdl.handle.net/1828/3604.

MLA Handbook (7th Edition):

Rocha, Bruno Filipe Ferreira Graca. “Structural health monitoring of aircraft structures: development of a phased array system.” 2011. Web. 31 Mar 2020.

Vancouver:

Rocha BFFG. Structural health monitoring of aircraft structures: development of a phased array system. [Internet] [Masters thesis]. University of Victoria; 2011. [cited 2020 Mar 31]. Available from: http://hdl.handle.net/1828/3604.

Council of Science Editors:

Rocha BFFG. Structural health monitoring of aircraft structures: development of a phased array system. [Masters Thesis]. University of Victoria; 2011. Available from: http://hdl.handle.net/1828/3604


Oregon State University

8. Gillins, Matthew N. Unmanned Aircraft Systems for Bridge Inspection : Testing and Developing End-to-End Operational Workflow.

Degree: MS, Civil Engineering, 2016, Oregon State University

 Bridge inspections are vital for monitoring the health and serviceability of transportation infrastructure throughout the world. However, inspections can be logistically-challenging, expensive, and dangerous. For… (more)

Subjects/Keywords: Bridge; Drone aircraft

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APA (6th Edition):

Gillins, M. N. (2016). Unmanned Aircraft Systems for Bridge Inspection : Testing and Developing End-to-End Operational Workflow. (Masters Thesis). Oregon State University. Retrieved from http://hdl.handle.net/1957/60001

Chicago Manual of Style (16th Edition):

Gillins, Matthew N. “Unmanned Aircraft Systems for Bridge Inspection : Testing and Developing End-to-End Operational Workflow.” 2016. Masters Thesis, Oregon State University. Accessed March 31, 2020. http://hdl.handle.net/1957/60001.

MLA Handbook (7th Edition):

Gillins, Matthew N. “Unmanned Aircraft Systems for Bridge Inspection : Testing and Developing End-to-End Operational Workflow.” 2016. Web. 31 Mar 2020.

Vancouver:

Gillins MN. Unmanned Aircraft Systems for Bridge Inspection : Testing and Developing End-to-End Operational Workflow. [Internet] [Masters thesis]. Oregon State University; 2016. [cited 2020 Mar 31]. Available from: http://hdl.handle.net/1957/60001.

Council of Science Editors:

Gillins MN. Unmanned Aircraft Systems for Bridge Inspection : Testing and Developing End-to-End Operational Workflow. [Masters Thesis]. Oregon State University; 2016. Available from: http://hdl.handle.net/1957/60001


Delft University of Technology

9. Van Bogaert, J. Assessment of Potential Fuel Saving Benefits of Hybrid-Electric Regional Aircraft:.

Degree: 2015, Delft University of Technology

 Both NASA and the EU have set ambitious goals in terms of aircraft emission reduction. Previous studies have indicated that these goals can not be… (more)

Subjects/Keywords: hybrid-electric; aircraft

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APA (6th Edition):

Van Bogaert, J. (2015). Assessment of Potential Fuel Saving Benefits of Hybrid-Electric Regional Aircraft:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:0fc7019f-d988-45c1-a7e2-55825f4f90ca

Chicago Manual of Style (16th Edition):

Van Bogaert, J. “Assessment of Potential Fuel Saving Benefits of Hybrid-Electric Regional Aircraft:.” 2015. Masters Thesis, Delft University of Technology. Accessed March 31, 2020. http://resolver.tudelft.nl/uuid:0fc7019f-d988-45c1-a7e2-55825f4f90ca.

MLA Handbook (7th Edition):

Van Bogaert, J. “Assessment of Potential Fuel Saving Benefits of Hybrid-Electric Regional Aircraft:.” 2015. Web. 31 Mar 2020.

Vancouver:

Van Bogaert J. Assessment of Potential Fuel Saving Benefits of Hybrid-Electric Regional Aircraft:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2020 Mar 31]. Available from: http://resolver.tudelft.nl/uuid:0fc7019f-d988-45c1-a7e2-55825f4f90ca.

Council of Science Editors:

Van Bogaert J. Assessment of Potential Fuel Saving Benefits of Hybrid-Electric Regional Aircraft:. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:0fc7019f-d988-45c1-a7e2-55825f4f90ca


Delft University of Technology

10. Le, N.T.P. The design of a next generation Y class aircraft seat:.

Degree: 2015, Delft University of Technology

 Globalization has resulted in an increase in demand for air travel, whether for business or for leisure. And this demand is expected to rise a… (more)

Subjects/Keywords: aircraft seat; design

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APA (6th Edition):

Le, N. T. P. (2015). The design of a next generation Y class aircraft seat:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:f4307eb4-f448-40d9-b65a-5a0a3356904f

Chicago Manual of Style (16th Edition):

Le, N T P. “The design of a next generation Y class aircraft seat:.” 2015. Masters Thesis, Delft University of Technology. Accessed March 31, 2020. http://resolver.tudelft.nl/uuid:f4307eb4-f448-40d9-b65a-5a0a3356904f.

MLA Handbook (7th Edition):

Le, N T P. “The design of a next generation Y class aircraft seat:.” 2015. Web. 31 Mar 2020.

Vancouver:

Le NTP. The design of a next generation Y class aircraft seat:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2020 Mar 31]. Available from: http://resolver.tudelft.nl/uuid:f4307eb4-f448-40d9-b65a-5a0a3356904f.

Council of Science Editors:

Le NTP. The design of a next generation Y class aircraft seat:. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:f4307eb4-f448-40d9-b65a-5a0a3356904f


San Jose State University

11. Hartney, Christopher. Design of a Small Solar-Powered Unmanned Aerial Vehicle.

Degree: MS, Mechanical and Aerospace Engineering, 2011, San Jose State University

  This thesis reports on a conceptual design of a solar-powered unmanned aerial vehicle (UAV) with a mass no more than 10 kg. This UAV… (more)

Subjects/Keywords: Aircraft; Solar; UAV

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APA (6th Edition):

Hartney, C. (2011). Design of a Small Solar-Powered Unmanned Aerial Vehicle. (Masters Thesis). San Jose State University. Retrieved from https://doi.org/10.31979/etd.2nzx-arxy ; https://scholarworks.sjsu.edu/etd_theses/4093

Chicago Manual of Style (16th Edition):

Hartney, Christopher. “Design of a Small Solar-Powered Unmanned Aerial Vehicle.” 2011. Masters Thesis, San Jose State University. Accessed March 31, 2020. https://doi.org/10.31979/etd.2nzx-arxy ; https://scholarworks.sjsu.edu/etd_theses/4093.

MLA Handbook (7th Edition):

Hartney, Christopher. “Design of a Small Solar-Powered Unmanned Aerial Vehicle.” 2011. Web. 31 Mar 2020.

Vancouver:

Hartney C. Design of a Small Solar-Powered Unmanned Aerial Vehicle. [Internet] [Masters thesis]. San Jose State University; 2011. [cited 2020 Mar 31]. Available from: https://doi.org/10.31979/etd.2nzx-arxy ; https://scholarworks.sjsu.edu/etd_theses/4093.

Council of Science Editors:

Hartney C. Design of a Small Solar-Powered Unmanned Aerial Vehicle. [Masters Thesis]. San Jose State University; 2011. Available from: https://doi.org/10.31979/etd.2nzx-arxy ; https://scholarworks.sjsu.edu/etd_theses/4093


University of Western Australia

12. Bryant, David. Design and prototyping of an aircraft to maximize the triaviation score.

Degree: M. Eng.Sci., 2008, University of Western Australia

This thesis describes some of the processes and results obtained during the design and prototyping of a single seat experimental aircraft. The major aim was… (more)

Subjects/Keywords: Airplanes; Research aircraft; Aircraft design; Triaviation score; Experimental aircraft

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APA (6th Edition):

Bryant, D. (2008). Design and prototyping of an aircraft to maximize the triaviation score. (Masters Thesis). University of Western Australia. Retrieved from http://repository.uwa.edu.au:80/R/?func=dbin-jump-full&object_id=6314&local_base=GEN01-INS01

Chicago Manual of Style (16th Edition):

Bryant, David. “Design and prototyping of an aircraft to maximize the triaviation score.” 2008. Masters Thesis, University of Western Australia. Accessed March 31, 2020. http://repository.uwa.edu.au:80/R/?func=dbin-jump-full&object_id=6314&local_base=GEN01-INS01.

MLA Handbook (7th Edition):

Bryant, David. “Design and prototyping of an aircraft to maximize the triaviation score.” 2008. Web. 31 Mar 2020.

Vancouver:

Bryant D. Design and prototyping of an aircraft to maximize the triaviation score. [Internet] [Masters thesis]. University of Western Australia; 2008. [cited 2020 Mar 31]. Available from: http://repository.uwa.edu.au:80/R/?func=dbin-jump-full&object_id=6314&local_base=GEN01-INS01.

Council of Science Editors:

Bryant D. Design and prototyping of an aircraft to maximize the triaviation score. [Masters Thesis]. University of Western Australia; 2008. Available from: http://repository.uwa.edu.au:80/R/?func=dbin-jump-full&object_id=6314&local_base=GEN01-INS01


University of Florida

13. Grant, Daniel. Modeling and Dynamic Analysis of a Multi-Joint Morphing Aircraft.

Degree: MS, Aerospace Engineering - Mechanical and Aerospace Engineering, 2009, University of Florida

 Morphing, which changes the shape and configuration of an aircraft, is being adopted to expand mission capabilities of aircraft. The introduction of biological-inspired morphing is… (more)

Subjects/Keywords: Aerodynamics; Aircraft; Aircraft maneuvers; Aircraft pitch; Aircraft roll; Aircraft wings; Altitude; Coordinate systems; Inertia; Sine function; daniel, grant, lind, morphing, uav

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APA (6th Edition):

Grant, D. (2009). Modeling and Dynamic Analysis of a Multi-Joint Morphing Aircraft. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0024477

Chicago Manual of Style (16th Edition):

Grant, Daniel. “Modeling and Dynamic Analysis of a Multi-Joint Morphing Aircraft.” 2009. Masters Thesis, University of Florida. Accessed March 31, 2020. http://ufdc.ufl.edu/UFE0024477.

MLA Handbook (7th Edition):

Grant, Daniel. “Modeling and Dynamic Analysis of a Multi-Joint Morphing Aircraft.” 2009. Web. 31 Mar 2020.

Vancouver:

Grant D. Modeling and Dynamic Analysis of a Multi-Joint Morphing Aircraft. [Internet] [Masters thesis]. University of Florida; 2009. [cited 2020 Mar 31]. Available from: http://ufdc.ufl.edu/UFE0024477.

Council of Science Editors:

Grant D. Modeling and Dynamic Analysis of a Multi-Joint Morphing Aircraft. [Masters Thesis]. University of Florida; 2009. Available from: http://ufdc.ufl.edu/UFE0024477


Texas A&M University

14. Niksch, Adam. Six Degree of Freedom Morphing Aircraft Dynamical Model with Aerodynamics.

Degree: 2010, Texas A&M University

 Morphing aircraft are envisioned to have multirole capability where the ability to change shape allows for adaptation to a changing mission environment. In order to… (more)

Subjects/Keywords: morphing; morphing aircraft model; aerodynamic morphing aircraft model; dynamical morphing aircraft model

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APA (6th Edition):

Niksch, A. (2010). Six Degree of Freedom Morphing Aircraft Dynamical Model with Aerodynamics. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2009-08-7180

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):

Niksch, Adam. “Six Degree of Freedom Morphing Aircraft Dynamical Model with Aerodynamics.” 2010. Thesis, Texas A&M University. Accessed March 31, 2020. http://hdl.handle.net/1969.1/ETD-TAMU-2009-08-7180.

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

MLA Handbook (7th Edition):

Niksch, Adam. “Six Degree of Freedom Morphing Aircraft Dynamical Model with Aerodynamics.” 2010. Web. 31 Mar 2020.

Vancouver:

Niksch A. Six Degree of Freedom Morphing Aircraft Dynamical Model with Aerodynamics. [Internet] [Thesis]. Texas A&M University; 2010. [cited 2020 Mar 31]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2009-08-7180.

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

Council of Science Editors:

Niksch A. Six Degree of Freedom Morphing Aircraft Dynamical Model with Aerodynamics. [Thesis]. Texas A&M University; 2010. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2009-08-7180

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

15. Al-Shamma, Omran. Development of Interactive Aircraft Design Software for Use in Problem Based Learning .

Degree: 2013, University of Hertfordshire

 In the last ten years or so, many interactive aircraft design software packages have been released into the market. One drawback of these packages is… (more)

Subjects/Keywords: Aircraft Design; Problem-Based Learning; Preliminary Aircraft Design; Aircraft Design Software; Weight Estimation; Cost Estimation

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APA (6th Edition):

Al-Shamma, O. (2013). Development of Interactive Aircraft Design Software for Use in Problem Based Learning . (Thesis). University of Hertfordshire. Retrieved from http://hdl.handle.net/2299/12108

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):

Al-Shamma, Omran. “Development of Interactive Aircraft Design Software for Use in Problem Based Learning .” 2013. Thesis, University of Hertfordshire. Accessed March 31, 2020. http://hdl.handle.net/2299/12108.

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

MLA Handbook (7th Edition):

Al-Shamma, Omran. “Development of Interactive Aircraft Design Software for Use in Problem Based Learning .” 2013. Web. 31 Mar 2020.

Vancouver:

Al-Shamma O. Development of Interactive Aircraft Design Software for Use in Problem Based Learning . [Internet] [Thesis]. University of Hertfordshire; 2013. [cited 2020 Mar 31]. Available from: http://hdl.handle.net/2299/12108.

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

Council of Science Editors:

Al-Shamma O. Development of Interactive Aircraft Design Software for Use in Problem Based Learning . [Thesis]. University of Hertfordshire; 2013. Available from: http://hdl.handle.net/2299/12108

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


Ryerson University

16. Simms, Devin. Lidar-based surface following control for unmanned aerial vehicles.

Degree: 2017, Ryerson University

 A simulation study is performed on a quadcopter which uses a LIDAR sensor to allow a quadcopter to navigate along and maintain a set distance… (more)

Subjects/Keywords: Drone aircraft  – Design and construction; Drone aircraft  – Control systems; Drone aircraft; Optical radar

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

APA (6th Edition):

Simms, D. (2017). Lidar-based surface following control for unmanned aerial vehicles. (Thesis). Ryerson University. Retrieved from https://digital.library.ryerson.ca/islandora/object/RULA%3A6636

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):

Simms, Devin. “Lidar-based surface following control for unmanned aerial vehicles.” 2017. Thesis, Ryerson University. Accessed March 31, 2020. https://digital.library.ryerson.ca/islandora/object/RULA%3A6636.

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

MLA Handbook (7th Edition):

Simms, Devin. “Lidar-based surface following control for unmanned aerial vehicles.” 2017. Web. 31 Mar 2020.

Vancouver:

Simms D. Lidar-based surface following control for unmanned aerial vehicles. [Internet] [Thesis]. Ryerson University; 2017. [cited 2020 Mar 31]. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A6636.

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

Council of Science Editors:

Simms D. Lidar-based surface following control for unmanned aerial vehicles. [Thesis]. Ryerson University; 2017. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A6636

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


Stellenbosch University

17. De Hart, Ruan Dirk. Advanced take-off and flight control algorithms for fixed wing unmanned aerial vehicles.

Degree: Electrical and Electronic Engineering, 2010, Stellenbosch University

Thesis (MScEng (Electrical and Electronic Engineering)) – University of Stellenbosch, 2010.

ENGLISH ABSTRACT: This thesis presents the development and implementation of a position based kinematic guidance… (more)

Subjects/Keywords: Electronic engineering; Drone aircraft  – Control systems; Drone aircraft  – Takeoff; Drone aircraft  – Landing

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APA (6th Edition):

De Hart, R. D. (2010). Advanced take-off and flight control algorithms for fixed wing unmanned aerial vehicles. (Thesis). Stellenbosch University. Retrieved from http://hdl.handle.net/10019.1/4179

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):

De Hart, Ruan Dirk. “Advanced take-off and flight control algorithms for fixed wing unmanned aerial vehicles.” 2010. Thesis, Stellenbosch University. Accessed March 31, 2020. http://hdl.handle.net/10019.1/4179.

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

MLA Handbook (7th Edition):

De Hart, Ruan Dirk. “Advanced take-off and flight control algorithms for fixed wing unmanned aerial vehicles.” 2010. Web. 31 Mar 2020.

Vancouver:

De Hart RD. Advanced take-off and flight control algorithms for fixed wing unmanned aerial vehicles. [Internet] [Thesis]. Stellenbosch University; 2010. [cited 2020 Mar 31]. Available from: http://hdl.handle.net/10019.1/4179.

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

Council of Science Editors:

De Hart RD. Advanced take-off and flight control algorithms for fixed wing unmanned aerial vehicles. [Thesis]. Stellenbosch University; 2010. Available from: http://hdl.handle.net/10019.1/4179

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


The Ohio State University

18. Robertson, Cole D. A Computational and Design Characterization for the Flowfield behind a C-130 during an Unmanned Aerial Vehicle Docking.

Degree: MS, Aero/Astro Engineering, 2019, The Ohio State University

 The complicated fluid interactions and wake dynamics generated astern of large cargo aircraft (such as Lockheed Martin’s C-130 Hercules) present concerns for standard and novel… (more)

Subjects/Keywords: Aerospace Engineering; UAV, aircraft design, aircraft control, aircraft stability, computational fluid dynamics

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APA (6th Edition):

Robertson, C. D. (2019). A Computational and Design Characterization for the Flowfield behind a C-130 during an Unmanned Aerial Vehicle Docking. (Masters Thesis). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1563533448658585

Chicago Manual of Style (16th Edition):

Robertson, Cole D. “A Computational and Design Characterization for the Flowfield behind a C-130 during an Unmanned Aerial Vehicle Docking.” 2019. Masters Thesis, The Ohio State University. Accessed March 31, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=osu1563533448658585.

MLA Handbook (7th Edition):

Robertson, Cole D. “A Computational and Design Characterization for the Flowfield behind a C-130 during an Unmanned Aerial Vehicle Docking.” 2019. Web. 31 Mar 2020.

Vancouver:

Robertson CD. A Computational and Design Characterization for the Flowfield behind a C-130 during an Unmanned Aerial Vehicle Docking. [Internet] [Masters thesis]. The Ohio State University; 2019. [cited 2020 Mar 31]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1563533448658585.

Council of Science Editors:

Robertson CD. A Computational and Design Characterization for the Flowfield behind a C-130 during an Unmanned Aerial Vehicle Docking. [Masters Thesis]. The Ohio State University; 2019. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1563533448658585

19. [No author]. Multidisciplinary Analysis of Closed, Nonplanar Wing Configurations for Transport Aircraft.

Degree: PhD, Mechanical Engineering/G??nie m??canique, 2016, Royal Military College of Canada

A multidisciplinary study of an unconventional aircraft configuration was undertaken to determine if such a design could decrease the environmental impact of civil air transportation… (more)

Subjects/Keywords: Aircraft design; Optimization; Nonplanar wings

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APA (6th Edition):

author], [. (2016). Multidisciplinary Analysis of Closed, Nonplanar Wing Configurations for Transport Aircraft. (Doctoral Dissertation). Royal Military College of Canada. Retrieved from http://hdl.handle.net/11264/981

Chicago Manual of Style (16th Edition):

author], [No. “Multidisciplinary Analysis of Closed, Nonplanar Wing Configurations for Transport Aircraft.” 2016. Doctoral Dissertation, Royal Military College of Canada. Accessed March 31, 2020. http://hdl.handle.net/11264/981.

MLA Handbook (7th Edition):

author], [No. “Multidisciplinary Analysis of Closed, Nonplanar Wing Configurations for Transport Aircraft.” 2016. Web. 31 Mar 2020.

Vancouver:

author] [. Multidisciplinary Analysis of Closed, Nonplanar Wing Configurations for Transport Aircraft. [Internet] [Doctoral dissertation]. Royal Military College of Canada; 2016. [cited 2020 Mar 31]. Available from: http://hdl.handle.net/11264/981.

Council of Science Editors:

author] [. Multidisciplinary Analysis of Closed, Nonplanar Wing Configurations for Transport Aircraft. [Doctoral Dissertation]. Royal Military College of Canada; 2016. Available from: http://hdl.handle.net/11264/981


Texas A&M University

20. Ding, Yuanyuan. Decentralized aircraft landing scheduling at single runway non-controlled airports.

Degree: 2009, Texas A&M University

 The existing air transportation system is approaching a bottleneck because its dominant huband- spoke model results in a concentration of a large percentage of the… (more)

Subjects/Keywords: Decentralize; Aircraft Landing Scheduling

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APA (6th Edition):

Ding, Y. (2009). Decentralized aircraft landing scheduling at single runway non-controlled airports. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1218

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):

Ding, Yuanyuan. “Decentralized aircraft landing scheduling at single runway non-controlled airports.” 2009. Thesis, Texas A&M University. Accessed March 31, 2020. http://hdl.handle.net/1969.1/ETD-TAMU-1218.

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

MLA Handbook (7th Edition):

Ding, Yuanyuan. “Decentralized aircraft landing scheduling at single runway non-controlled airports.” 2009. Web. 31 Mar 2020.

Vancouver:

Ding Y. Decentralized aircraft landing scheduling at single runway non-controlled airports. [Internet] [Thesis]. Texas A&M University; 2009. [cited 2020 Mar 31]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1218.

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

Council of Science Editors:

Ding Y. Decentralized aircraft landing scheduling at single runway non-controlled airports. [Thesis]. Texas A&M University; 2009. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1218

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


Anna University

21. Chinnaiyan, R. Investigations on reliability evaluation Of component based software systems; -.

Degree: Science and Humanities, 2014, Anna University

Software Component plays a predominant role in our day to day life newlineHome appliances medical diagnostic devices automated teller machines newlineAircrafts automobiles and mobile phones… (more)

Subjects/Keywords: Aircraft control systems; Aircrafts automobiles

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APA (6th Edition):

Chinnaiyan, R. (2014). Investigations on reliability evaluation Of component based software systems; -. (Thesis). Anna University. Retrieved from http://shodhganga.inflibnet.ac.in/handle/10603/25226

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):

Chinnaiyan, R. “Investigations on reliability evaluation Of component based software systems; -.” 2014. Thesis, Anna University. Accessed March 31, 2020. http://shodhganga.inflibnet.ac.in/handle/10603/25226.

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

MLA Handbook (7th Edition):

Chinnaiyan, R. “Investigations on reliability evaluation Of component based software systems; -.” 2014. Web. 31 Mar 2020.

Vancouver:

Chinnaiyan R. Investigations on reliability evaluation Of component based software systems; -. [Internet] [Thesis]. Anna University; 2014. [cited 2020 Mar 31]. Available from: http://shodhganga.inflibnet.ac.in/handle/10603/25226.

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

Council of Science Editors:

Chinnaiyan R. Investigations on reliability evaluation Of component based software systems; -. [Thesis]. Anna University; 2014. Available from: http://shodhganga.inflibnet.ac.in/handle/10603/25226

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


Penn State University

22. Harkins, Joseph. Automatic Controller Synthesis for a Reconfigurable UAV.

Degree: 2017, Penn State University

 This thesis describes the development of an adaptable control architecture that can be used to automatically synthesize inner-loop controllers for new configurations of modular aircraft.… (more)

Subjects/Keywords: Modular Aircraft; UAV; Controls; Aerodynamics

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APA (6th Edition):

Harkins, J. (2017). Automatic Controller Synthesis for a Reconfigurable UAV. (Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/13996jvh5789

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):

Harkins, Joseph. “Automatic Controller Synthesis for a Reconfigurable UAV.” 2017. Thesis, Penn State University. Accessed March 31, 2020. https://etda.libraries.psu.edu/catalog/13996jvh5789.

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

MLA Handbook (7th Edition):

Harkins, Joseph. “Automatic Controller Synthesis for a Reconfigurable UAV.” 2017. Web. 31 Mar 2020.

Vancouver:

Harkins J. Automatic Controller Synthesis for a Reconfigurable UAV. [Internet] [Thesis]. Penn State University; 2017. [cited 2020 Mar 31]. Available from: https://etda.libraries.psu.edu/catalog/13996jvh5789.

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

Council of Science Editors:

Harkins J. Automatic Controller Synthesis for a Reconfigurable UAV. [Thesis]. Penn State University; 2017. Available from: https://etda.libraries.psu.edu/catalog/13996jvh5789

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


University of Florida

23. Pasiliao, Crystal. Temporal Analysis of Transonic Flow Field Characteristics Associated with Limit Cycle Oscillations.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2009, University of Florida

 Limit Cycle Oscillation (LCO) is a sustained, non-divergent, periodic motion experienced by aircraft with certain external store configurations. Flutter, an instability caused by the aerodynamic… (more)

Subjects/Keywords: Aerodynamics; Aircraft; Aircraft pitch; Aircraft roll; Aircraft wings; Charge flow devices; Fast Fourier transformations; Limit cycles; Oscillation; Transonic flow

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APA (6th Edition):

Pasiliao, C. (2009). Temporal Analysis of Transonic Flow Field Characteristics Associated with Limit Cycle Oscillations. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0024231

Chicago Manual of Style (16th Edition):

Pasiliao, Crystal. “Temporal Analysis of Transonic Flow Field Characteristics Associated with Limit Cycle Oscillations.” 2009. Doctoral Dissertation, University of Florida. Accessed March 31, 2020. http://ufdc.ufl.edu/UFE0024231.

MLA Handbook (7th Edition):

Pasiliao, Crystal. “Temporal Analysis of Transonic Flow Field Characteristics Associated with Limit Cycle Oscillations.” 2009. Web. 31 Mar 2020.

Vancouver:

Pasiliao C. Temporal Analysis of Transonic Flow Field Characteristics Associated with Limit Cycle Oscillations. [Internet] [Doctoral dissertation]. University of Florida; 2009. [cited 2020 Mar 31]. Available from: http://ufdc.ufl.edu/UFE0024231.

Council of Science Editors:

Pasiliao C. Temporal Analysis of Transonic Flow Field Characteristics Associated with Limit Cycle Oscillations. [Doctoral Dissertation]. University of Florida; 2009. Available from: http://ufdc.ufl.edu/UFE0024231


Penn State University

24. Dunkin, Bradley Mark. DIRECTIVITY AND SPECTRAL SOURCE NOISE CHARACTERIZATION OF COMMERCIAL AIRCRAFT DURING LANDING WITH THRUST REVERSER ENGAGEMENT.

Degree: MS, Acoustics, 2008, Penn State University

 Recordings of aircraft landing operations have been analyzed to obtain directivity and spectral characteristics of the noise emitted during landing with thrust reversers engaged. The… (more)

Subjects/Keywords: aircraft noise; Community noise

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APA (6th Edition):

Dunkin, B. M. (2008). DIRECTIVITY AND SPECTRAL SOURCE NOISE CHARACTERIZATION OF COMMERCIAL AIRCRAFT DURING LANDING WITH THRUST REVERSER ENGAGEMENT. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/8400

Chicago Manual of Style (16th Edition):

Dunkin, Bradley Mark. “DIRECTIVITY AND SPECTRAL SOURCE NOISE CHARACTERIZATION OF COMMERCIAL AIRCRAFT DURING LANDING WITH THRUST REVERSER ENGAGEMENT.” 2008. Masters Thesis, Penn State University. Accessed March 31, 2020. https://etda.libraries.psu.edu/catalog/8400.

MLA Handbook (7th Edition):

Dunkin, Bradley Mark. “DIRECTIVITY AND SPECTRAL SOURCE NOISE CHARACTERIZATION OF COMMERCIAL AIRCRAFT DURING LANDING WITH THRUST REVERSER ENGAGEMENT.” 2008. Web. 31 Mar 2020.

Vancouver:

Dunkin BM. DIRECTIVITY AND SPECTRAL SOURCE NOISE CHARACTERIZATION OF COMMERCIAL AIRCRAFT DURING LANDING WITH THRUST REVERSER ENGAGEMENT. [Internet] [Masters thesis]. Penn State University; 2008. [cited 2020 Mar 31]. Available from: https://etda.libraries.psu.edu/catalog/8400.

Council of Science Editors:

Dunkin BM. DIRECTIVITY AND SPECTRAL SOURCE NOISE CHARACTERIZATION OF COMMERCIAL AIRCRAFT DURING LANDING WITH THRUST REVERSER ENGAGEMENT. [Masters Thesis]. Penn State University; 2008. Available from: https://etda.libraries.psu.edu/catalog/8400


Ryerson University

25. George, Issi-Rae Emanuelle. A multirotor vehicle performance prediction method.

Degree: 2017, Ryerson University

 A method has been developed to predict the performance of small multirotor vehicles. Using the vehicle geometry, rotor geometry and flight conditions as inputs, the… (more)

Subjects/Keywords: Drone aircraft  – Design and construction; Drone aircraft  – Flight testing; Drone aircraft  – Testing; Drone aircraft  – Aerodynamics; Rotors  – Aerodynamics  – Mathematical models; Rotors  – Testing

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APA (6th Edition):

George, I. E. (2017). A multirotor vehicle performance prediction method. (Thesis). Ryerson University. Retrieved from https://digital.library.ryerson.ca/islandora/object/RULA%3A6879

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):

George, Issi-Rae Emanuelle. “A multirotor vehicle performance prediction method.” 2017. Thesis, Ryerson University. Accessed March 31, 2020. https://digital.library.ryerson.ca/islandora/object/RULA%3A6879.

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

MLA Handbook (7th Edition):

George, Issi-Rae Emanuelle. “A multirotor vehicle performance prediction method.” 2017. Web. 31 Mar 2020.

Vancouver:

George IE. A multirotor vehicle performance prediction method. [Internet] [Thesis]. Ryerson University; 2017. [cited 2020 Mar 31]. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A6879.

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

Council of Science Editors:

George IE. A multirotor vehicle performance prediction method. [Thesis]. Ryerson University; 2017. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A6879

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


University of Florida

26. GRANT,DANIEL THURMOND. A Linear Input-Varying Framework for Modeling and Control of Morphing Aircraft.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2011, University of Florida

 Morphing, which changes the shape and configuration of an aircraft, is being adopted to expand mission capabilities of aircraft. The introduction of biological-inspired morphing is… (more)

Subjects/Keywords: Aircraft; Aircraft maneuvers; Aircraft wings; Damping; Eigenvectors; Inertia; Polynomials; Sine function; Trajectories; Velocity; AIRCRAFT  – CONTROL  – DYNAMICS  – MORPHING  – UNMANNED

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APA (6th Edition):

THURMOND, G. (2011). A Linear Input-Varying Framework for Modeling and Control of Morphing Aircraft. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0042424

Chicago Manual of Style (16th Edition):

THURMOND, GRANT,DANIEL. “A Linear Input-Varying Framework for Modeling and Control of Morphing Aircraft.” 2011. Doctoral Dissertation, University of Florida. Accessed March 31, 2020. http://ufdc.ufl.edu/UFE0042424.

MLA Handbook (7th Edition):

THURMOND, GRANT,DANIEL. “A Linear Input-Varying Framework for Modeling and Control of Morphing Aircraft.” 2011. Web. 31 Mar 2020.

Vancouver:

THURMOND G. A Linear Input-Varying Framework for Modeling and Control of Morphing Aircraft. [Internet] [Doctoral dissertation]. University of Florida; 2011. [cited 2020 Mar 31]. Available from: http://ufdc.ufl.edu/UFE0042424.

Council of Science Editors:

THURMOND G. A Linear Input-Varying Framework for Modeling and Control of Morphing Aircraft. [Doctoral Dissertation]. University of Florida; 2011. Available from: http://ufdc.ufl.edu/UFE0042424


Virginia Tech

27. Freire Burgos, Edwin R. Aviation Global Demand Forecast Model Development: Air Transportation Demand Distribution and Aircraft Fleet Evolution.

Degree: MS, Civil and Environmental Engineering, 2017, Virginia Tech

 The Portfolio Analysis Management Office (PAMO) for the Aeronautics Research Mission Directorate (ARMD) at NASA Headquarters tasked the Systems Analysis and Concepts Directorate at NASA… (more)

Subjects/Keywords: Air Travel Demand; Fratar Model; Trip Distribution; Worldwide Aircraft Fleet; Aircraft Fleet Evolution; New Generation Aircraft; NASA’s Advanced Technology Aircraft

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APA (6th Edition):

Freire Burgos, E. R. (2017). Aviation Global Demand Forecast Model Development: Air Transportation Demand Distribution and Aircraft Fleet Evolution. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/81313

Chicago Manual of Style (16th Edition):

Freire Burgos, Edwin R. “Aviation Global Demand Forecast Model Development: Air Transportation Demand Distribution and Aircraft Fleet Evolution.” 2017. Masters Thesis, Virginia Tech. Accessed March 31, 2020. http://hdl.handle.net/10919/81313.

MLA Handbook (7th Edition):

Freire Burgos, Edwin R. “Aviation Global Demand Forecast Model Development: Air Transportation Demand Distribution and Aircraft Fleet Evolution.” 2017. Web. 31 Mar 2020.

Vancouver:

Freire Burgos ER. Aviation Global Demand Forecast Model Development: Air Transportation Demand Distribution and Aircraft Fleet Evolution. [Internet] [Masters thesis]. Virginia Tech; 2017. [cited 2020 Mar 31]. Available from: http://hdl.handle.net/10919/81313.

Council of Science Editors:

Freire Burgos ER. Aviation Global Demand Forecast Model Development: Air Transportation Demand Distribution and Aircraft Fleet Evolution. [Masters Thesis]. Virginia Tech; 2017. Available from: http://hdl.handle.net/10919/81313


Oregon State University

28. Routledge, Garry L. A paradigmatic framework for flight safety.

Degree: PhD, Industrial and Manufacturing Engineering, 1991, Oregon State University

 Statistically, travel by air is one of the safest forms of transportation. Yet we continue to experience aviation tragedies. Do we fully understand flight safety… (more)

Subjects/Keywords: Aircraft accidents

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APA (6th Edition):

Routledge, G. L. (1991). A paradigmatic framework for flight safety. (Doctoral Dissertation). Oregon State University. Retrieved from http://hdl.handle.net/1957/37472

Chicago Manual of Style (16th Edition):

Routledge, Garry L. “A paradigmatic framework for flight safety.” 1991. Doctoral Dissertation, Oregon State University. Accessed March 31, 2020. http://hdl.handle.net/1957/37472.

MLA Handbook (7th Edition):

Routledge, Garry L. “A paradigmatic framework for flight safety.” 1991. Web. 31 Mar 2020.

Vancouver:

Routledge GL. A paradigmatic framework for flight safety. [Internet] [Doctoral dissertation]. Oregon State University; 1991. [cited 2020 Mar 31]. Available from: http://hdl.handle.net/1957/37472.

Council of Science Editors:

Routledge GL. A paradigmatic framework for flight safety. [Doctoral Dissertation]. Oregon State University; 1991. Available from: http://hdl.handle.net/1957/37472


Oregon State University

29. Bell, Adam R. Learning-based control and coordination of autonomous UAVs.

Degree: MS, Mechanical Engineering, 2010, Oregon State University

 Uninhabited aerial vehicles, also called UAVs are currently controller by a combination of a human pilot at a remote location, and autopilot systems similar to… (more)

Subjects/Keywords: coordination; Drone aircraft  – Control systems

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APA (6th Edition):

Bell, A. R. (2010). Learning-based control and coordination of autonomous UAVs. (Masters Thesis). Oregon State University. Retrieved from http://hdl.handle.net/1957/19597

Chicago Manual of Style (16th Edition):

Bell, Adam R. “Learning-based control and coordination of autonomous UAVs.” 2010. Masters Thesis, Oregon State University. Accessed March 31, 2020. http://hdl.handle.net/1957/19597.

MLA Handbook (7th Edition):

Bell, Adam R. “Learning-based control and coordination of autonomous UAVs.” 2010. Web. 31 Mar 2020.

Vancouver:

Bell AR. Learning-based control and coordination of autonomous UAVs. [Internet] [Masters thesis]. Oregon State University; 2010. [cited 2020 Mar 31]. Available from: http://hdl.handle.net/1957/19597.

Council of Science Editors:

Bell AR. Learning-based control and coordination of autonomous UAVs. [Masters Thesis]. Oregon State University; 2010. Available from: http://hdl.handle.net/1957/19597


Virginia Tech

30. Parsons, Shawn M. Strain-based Topology Optimization of a 2D Morphing Transitional Surface.

Degree: MS, Aerospace and Ocean Engineering, 2018, Virginia Tech

 Morphing aircraft offer many benefits. However, the design of stiff yet flexible structures still provides many obstacles to fully exploring and realizing morphing structures. Due… (more)

Subjects/Keywords: Topology; structures; morphing aircraft

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APA (6th Edition):

Parsons, S. M. (2018). Strain-based Topology Optimization of a 2D Morphing Transitional Surface. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/83961

Chicago Manual of Style (16th Edition):

Parsons, Shawn M. “Strain-based Topology Optimization of a 2D Morphing Transitional Surface.” 2018. Masters Thesis, Virginia Tech. Accessed March 31, 2020. http://hdl.handle.net/10919/83961.

MLA Handbook (7th Edition):

Parsons, Shawn M. “Strain-based Topology Optimization of a 2D Morphing Transitional Surface.” 2018. Web. 31 Mar 2020.

Vancouver:

Parsons SM. Strain-based Topology Optimization of a 2D Morphing Transitional Surface. [Internet] [Masters thesis]. Virginia Tech; 2018. [cited 2020 Mar 31]. Available from: http://hdl.handle.net/10919/83961.

Council of Science Editors:

Parsons SM. Strain-based Topology Optimization of a 2D Morphing Transitional Surface. [Masters Thesis]. Virginia Tech; 2018. Available from: http://hdl.handle.net/10919/83961

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