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You searched for subject:(unmanned aircraft). Showing records 1 – 30 of 142 total matches.

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Stellenbosch University

1. 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 April 22, 2019. 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. 22 Apr 2019.

Vancouver:

Maneschijn A. A framework and criteria for the operability of unmanned aircraft systems. [Internet] [Thesis]. Stellenbosch University; 2010. [cited 2019 Apr 22]. 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


Louisiana State University

2. King, Sean Lauderdale. Design and Performance Estimation of a Low-Reynolds Number Unmanned Aircraft System.

Degree: MSME, Aerodynamics and Fluid Mechanics, 2018, Louisiana State University

  The purpose of this thesis is to conceptually design a fixed-wing unmanned aircraft systems (UAS) with a higher flight-time and top stable speed than… (more)

Subjects/Keywords: Design; Aerodynamics; Control; Unmanned Aircraft System

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APA (6th Edition):

King, S. L. (2018). Design and Performance Estimation of a Low-Reynolds Number Unmanned Aircraft System. (Masters Thesis). Louisiana State University. Retrieved from https://digitalcommons.lsu.edu/gradschool_theses/4773

Chicago Manual of Style (16th Edition):

King, Sean Lauderdale. “Design and Performance Estimation of a Low-Reynolds Number Unmanned Aircraft System.” 2018. Masters Thesis, Louisiana State University. Accessed April 22, 2019. https://digitalcommons.lsu.edu/gradschool_theses/4773.

MLA Handbook (7th Edition):

King, Sean Lauderdale. “Design and Performance Estimation of a Low-Reynolds Number Unmanned Aircraft System.” 2018. Web. 22 Apr 2019.

Vancouver:

King SL. Design and Performance Estimation of a Low-Reynolds Number Unmanned Aircraft System. [Internet] [Masters thesis]. Louisiana State University; 2018. [cited 2019 Apr 22]. Available from: https://digitalcommons.lsu.edu/gradschool_theses/4773.

Council of Science Editors:

King SL. Design and Performance Estimation of a Low-Reynolds Number Unmanned Aircraft System. [Masters Thesis]. Louisiana State University; 2018. Available from: https://digitalcommons.lsu.edu/gradschool_theses/4773


University of Illinois – Urbana-Champaign

3. Hanley, David John. An improved model-based observer for inertial navigation for quadrotors with low cost IMUs.

Degree: MS, Aerospace Engineering, 2015, University of Illinois – Urbana-Champaign

 In this thesis, we present a model-based observer for inertial navigation of quadrotors and other multirotor aircraft. We include in our model a Coriolis term… (more)

Subjects/Keywords: Inertial Navigation; Unmanned Aircraft; Quadrotors; Observer; Estimator

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APA (6th Edition):

Hanley, D. J. (2015). An improved model-based observer for inertial navigation for quadrotors with low cost IMUs. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/88007

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):

Hanley, David John. “An improved model-based observer for inertial navigation for quadrotors with low cost IMUs.” 2015. Thesis, University of Illinois – Urbana-Champaign. Accessed April 22, 2019. http://hdl.handle.net/2142/88007.

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

MLA Handbook (7th Edition):

Hanley, David John. “An improved model-based observer for inertial navigation for quadrotors with low cost IMUs.” 2015. Web. 22 Apr 2019.

Vancouver:

Hanley DJ. An improved model-based observer for inertial navigation for quadrotors with low cost IMUs. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2015. [cited 2019 Apr 22]. Available from: http://hdl.handle.net/2142/88007.

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

Council of Science Editors:

Hanley DJ. An improved model-based observer for inertial navigation for quadrotors with low cost IMUs. [Thesis]. University of Illinois – Urbana-Champaign; 2015. Available from: http://hdl.handle.net/2142/88007

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


University of Dayton

4. Landolfo, Giuseppe. Aerodynamic and Structural Design of a Small Nonplanar Wing UAV.

Degree: MS(M.S.), Aerospace Engineering, 2008, University of Dayton

 The overall air vehicle performance of a multiple lifting surface configuration has been studied with respect to both structural and aerodynamic considerations for a candidate… (more)

Subjects/Keywords: Engineering; Aerospace; aircraft design; aerodynamics; structural analysis; UAV; unmanned aircraft; biplane

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APA (6th Edition):

Landolfo, G. (2008). Aerodynamic and Structural Design of a Small Nonplanar Wing UAV. (Masters Thesis). University of Dayton. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=dayton1262089704

Chicago Manual of Style (16th Edition):

Landolfo, Giuseppe. “Aerodynamic and Structural Design of a Small Nonplanar Wing UAV.” 2008. Masters Thesis, University of Dayton. Accessed April 22, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=dayton1262089704.

MLA Handbook (7th Edition):

Landolfo, Giuseppe. “Aerodynamic and Structural Design of a Small Nonplanar Wing UAV.” 2008. Web. 22 Apr 2019.

Vancouver:

Landolfo G. Aerodynamic and Structural Design of a Small Nonplanar Wing UAV. [Internet] [Masters thesis]. University of Dayton; 2008. [cited 2019 Apr 22]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=dayton1262089704.

Council of Science Editors:

Landolfo G. Aerodynamic and Structural Design of a Small Nonplanar Wing UAV. [Masters Thesis]. University of Dayton; 2008. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=dayton1262089704


University of Johannesburg

5. Wilkins, Grant. Design and implementation of a power system for a solar unmanned aerial vehicle.

Degree: 2012, University of Johannesburg

M. Ing.

Solar powered UAV's have gained world wide attention with aircraft such as Solar Impulse and Quinetiq's Zephyr. UAV's in general are becomming increasingly… (more)

Subjects/Keywords: Solar aircraft; Drone aircraft; Unmanned aerial vehicle; Solar power system design

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APA (6th Edition):

Wilkins, G. (2012). Design and implementation of a power system for a solar unmanned aerial vehicle. (Thesis). University of Johannesburg. Retrieved from http://hdl.handle.net/10210/4835

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):

Wilkins, Grant. “Design and implementation of a power system for a solar unmanned aerial vehicle.” 2012. Thesis, University of Johannesburg. Accessed April 22, 2019. http://hdl.handle.net/10210/4835.

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

MLA Handbook (7th Edition):

Wilkins, Grant. “Design and implementation of a power system for a solar unmanned aerial vehicle.” 2012. Web. 22 Apr 2019.

Vancouver:

Wilkins G. Design and implementation of a power system for a solar unmanned aerial vehicle. [Internet] [Thesis]. University of Johannesburg; 2012. [cited 2019 Apr 22]. Available from: http://hdl.handle.net/10210/4835.

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

Council of Science Editors:

Wilkins G. Design and implementation of a power system for a solar unmanned aerial vehicle. [Thesis]. University of Johannesburg; 2012. Available from: http://hdl.handle.net/10210/4835

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


University of Florida

6. 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 April 22, 2019. 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. 22 Apr 2019.

Vancouver:

THURMOND G. A Linear Input-Varying Framework for Modeling and Control of Morphing Aircraft. [Internet] [Doctoral dissertation]. University of Florida; 2011. [cited 2019 Apr 22]. 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


Stellenbosch University

7. Meredith, Andre Paul. An unmanned aircraft system for maritime search and rescue.

Degree: Electrical and Electronic Engineering, 2011, Stellenbosch University

Thesis (MScEng (Electrical and Electronic Engineering)) – University of Stellenbosch, 2011.

ENGLISH ABSTRACT: Search and Rescue is an essential service provided by States and Militaries to… (more)

Subjects/Keywords: Electronic engineering; Drone aircraft; Search and rescue operations; Unmanned Aircraft System (UAF); Drone aircraft  – Rescue work

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APA (6th Edition):

Meredith, A. P. (2011). An unmanned aircraft system for maritime search and rescue. (Thesis). Stellenbosch University. Retrieved from http://hdl.handle.net/10019.1/6720

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):

Meredith, Andre Paul. “An unmanned aircraft system for maritime search and rescue.” 2011. Thesis, Stellenbosch University. Accessed April 22, 2019. http://hdl.handle.net/10019.1/6720.

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

MLA Handbook (7th Edition):

Meredith, Andre Paul. “An unmanned aircraft system for maritime search and rescue.” 2011. Web. 22 Apr 2019.

Vancouver:

Meredith AP. An unmanned aircraft system for maritime search and rescue. [Internet] [Thesis]. Stellenbosch University; 2011. [cited 2019 Apr 22]. Available from: http://hdl.handle.net/10019.1/6720.

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

Council of Science Editors:

Meredith AP. An unmanned aircraft system for maritime search and rescue. [Thesis]. Stellenbosch University; 2011. Available from: http://hdl.handle.net/10019.1/6720

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


Virginia Commonwealth University

8. Bakker, Tim. Dynamic Task-Allocation for Unmanned Aircraft Systems.

Degree: PhD, Engineering, 2014, Virginia Commonwealth University

 This dissertation addresses improvements to a consensus based task allocation algorithms for improving the Quality of Service in multi-task and multi-agent environments. Research in the… (more)

Subjects/Keywords: task-allocation; unmanned aircraft system; intelligent agent; collaborative; Engineering

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APA (6th Edition):

Bakker, T. (2014). Dynamic Task-Allocation for Unmanned Aircraft Systems. (Doctoral Dissertation). Virginia Commonwealth University. Retrieved from https://scholarscompass.vcu.edu/etd/3394

Chicago Manual of Style (16th Edition):

Bakker, Tim. “Dynamic Task-Allocation for Unmanned Aircraft Systems.” 2014. Doctoral Dissertation, Virginia Commonwealth University. Accessed April 22, 2019. https://scholarscompass.vcu.edu/etd/3394.

MLA Handbook (7th Edition):

Bakker, Tim. “Dynamic Task-Allocation for Unmanned Aircraft Systems.” 2014. Web. 22 Apr 2019.

Vancouver:

Bakker T. Dynamic Task-Allocation for Unmanned Aircraft Systems. [Internet] [Doctoral dissertation]. Virginia Commonwealth University; 2014. [cited 2019 Apr 22]. Available from: https://scholarscompass.vcu.edu/etd/3394.

Council of Science Editors:

Bakker T. Dynamic Task-Allocation for Unmanned Aircraft Systems. [Doctoral Dissertation]. Virginia Commonwealth University; 2014. Available from: https://scholarscompass.vcu.edu/etd/3394


University of Colorado

9. Weibel, Douglas E. Improving the accuracy of in-situ lower ABL wind measurements using sUAS.

Degree: PhD, Aerospace Engineering Sciences, 2015, University of Colorado

  Wind measurement is a challenging problem as wind is a spatiotemporal vector field and obtaining a set of measurements with desired spatial and temporal… (more)

Subjects/Keywords: UAS; UAV; Unmanned Aircraft; wind velocity; Aerospace Engineering; Environmental Sciences; Robotics

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APA (6th Edition):

Weibel, D. E. (2015). Improving the accuracy of in-situ lower ABL wind measurements using sUAS. (Doctoral Dissertation). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/105

Chicago Manual of Style (16th Edition):

Weibel, Douglas E. “Improving the accuracy of in-situ lower ABL wind measurements using sUAS.” 2015. Doctoral Dissertation, University of Colorado. Accessed April 22, 2019. http://scholar.colorado.edu/asen_gradetds/105.

MLA Handbook (7th Edition):

Weibel, Douglas E. “Improving the accuracy of in-situ lower ABL wind measurements using sUAS.” 2015. Web. 22 Apr 2019.

Vancouver:

Weibel DE. Improving the accuracy of in-situ lower ABL wind measurements using sUAS. [Internet] [Doctoral dissertation]. University of Colorado; 2015. [cited 2019 Apr 22]. Available from: http://scholar.colorado.edu/asen_gradetds/105.

Council of Science Editors:

Weibel DE. Improving the accuracy of in-situ lower ABL wind measurements using sUAS. [Doctoral Dissertation]. University of Colorado; 2015. Available from: http://scholar.colorado.edu/asen_gradetds/105

10. Lundmark, Johan. Utvärdering av digitala terrängmodeller framtagna med flygburen laserskanning och UAS-fotogrammetri.

Degree: GIS, 2018, University of Gävle

Over the last years there has been a rapid development in the UAS-technology (Unmanned Aircraft Systems) and today there are several UAS systems on… (more)

Subjects/Keywords: Airborne Laser Scanning (ALS); Digital Terrain Model (DTM); Unmanned Aircraft System (UAS); Unmanned Aircraft Vehicle (UAV); Digital terrängmodell (DTM); Flygburen laserskanning (FLS); Unmanned Aircraft System (UAS); Unmanned Aircraft Vehicle (UAV); Other Civil Engineering; Annan samhällsbyggnadsteknik

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APA (6th Edition):

Lundmark, J. (2018). Utvärdering av digitala terrängmodeller framtagna med flygburen laserskanning och UAS-fotogrammetri. (Thesis). University of Gävle. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:hig:diva-27295

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):

Lundmark, Johan. “Utvärdering av digitala terrängmodeller framtagna med flygburen laserskanning och UAS-fotogrammetri.” 2018. Thesis, University of Gävle. Accessed April 22, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:hig:diva-27295.

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

MLA Handbook (7th Edition):

Lundmark, Johan. “Utvärdering av digitala terrängmodeller framtagna med flygburen laserskanning och UAS-fotogrammetri.” 2018. Web. 22 Apr 2019.

Vancouver:

Lundmark J. Utvärdering av digitala terrängmodeller framtagna med flygburen laserskanning och UAS-fotogrammetri. [Internet] [Thesis]. University of Gävle; 2018. [cited 2019 Apr 22]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:hig:diva-27295.

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

Council of Science Editors:

Lundmark J. Utvärdering av digitala terrängmodeller framtagna med flygburen laserskanning och UAS-fotogrammetri. [Thesis]. University of Gävle; 2018. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:hig:diva-27295

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


University of California – Berkeley

11. Chandler, Katherine Fehr. Drone Flight and Failure: the United States' Secret Trials, Experiments and Operations in Unmanning, 1936-1973.

Degree: Rhetoric, 2014, University of California – Berkeley

 I examine the precursors to contemporary unmanned combat air vehicles (UCAVs) to ask what is at stake in the designation "unmanned?" The apparent misnomer dissociates… (more)

Subjects/Keywords: Rhetoric; American studies; Geography; Drones; Reconnaissance; Targeting; Unmanned Aircraft

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APA (6th Edition):

Chandler, K. F. (2014). Drone Flight and Failure: the United States' Secret Trials, Experiments and Operations in Unmanning, 1936-1973. (Thesis). University of California – Berkeley. Retrieved from http://www.escholarship.org/uc/item/0fg216f7

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):

Chandler, Katherine Fehr. “Drone Flight and Failure: the United States' Secret Trials, Experiments and Operations in Unmanning, 1936-1973.” 2014. Thesis, University of California – Berkeley. Accessed April 22, 2019. http://www.escholarship.org/uc/item/0fg216f7.

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

MLA Handbook (7th Edition):

Chandler, Katherine Fehr. “Drone Flight and Failure: the United States' Secret Trials, Experiments and Operations in Unmanning, 1936-1973.” 2014. Web. 22 Apr 2019.

Vancouver:

Chandler KF. Drone Flight and Failure: the United States' Secret Trials, Experiments and Operations in Unmanning, 1936-1973. [Internet] [Thesis]. University of California – Berkeley; 2014. [cited 2019 Apr 22]. Available from: http://www.escholarship.org/uc/item/0fg216f7.

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

Council of Science Editors:

Chandler KF. Drone Flight and Failure: the United States' Secret Trials, Experiments and Operations in Unmanning, 1936-1973. [Thesis]. University of California – Berkeley; 2014. Available from: http://www.escholarship.org/uc/item/0fg216f7

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


University of Newcastle

12. de Lamberterie, Pierre. A probabilistic framework for the assessment of robust autonomy in unmanned aircraft systems.

Degree: PhD, 2013, University of Newcastle

Research Doctorate - Doctor of Philosophy (PhD)

In the near future, Uninhabited Aircraft Systems (UAS) will bring significant benefits to a rapidly growing number of… (more)

Subjects/Keywords: unmanned aircraft systems; robust autonomy; fault tolerant systems; national airspace system

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APA (6th Edition):

de Lamberterie, P. (2013). A probabilistic framework for the assessment of robust autonomy in unmanned aircraft systems. (Doctoral Dissertation). University of Newcastle. Retrieved from http://hdl.handle.net/1959.13/1036693

Chicago Manual of Style (16th Edition):

de Lamberterie, Pierre. “A probabilistic framework for the assessment of robust autonomy in unmanned aircraft systems.” 2013. Doctoral Dissertation, University of Newcastle. Accessed April 22, 2019. http://hdl.handle.net/1959.13/1036693.

MLA Handbook (7th Edition):

de Lamberterie, Pierre. “A probabilistic framework for the assessment of robust autonomy in unmanned aircraft systems.” 2013. Web. 22 Apr 2019.

Vancouver:

de Lamberterie P. A probabilistic framework for the assessment of robust autonomy in unmanned aircraft systems. [Internet] [Doctoral dissertation]. University of Newcastle; 2013. [cited 2019 Apr 22]. Available from: http://hdl.handle.net/1959.13/1036693.

Council of Science Editors:

de Lamberterie P. A probabilistic framework for the assessment of robust autonomy in unmanned aircraft systems. [Doctoral Dissertation]. University of Newcastle; 2013. Available from: http://hdl.handle.net/1959.13/1036693


University of Victoria

13. Richards, Jenner. An Experimental Investigation of a Joined Wing Aircraft Configuration Using Flexible, Reduced Scale Flight Test Vehicles.

Degree: Department of Mechanical Engineering, 2014, University of Victoria

 The United States Air Force has specified a need for the next generation, High Altitude, Long Endurance aircraft capable of carrying advanced sensor arrays over… (more)

Subjects/Keywords: Aeroelastic; Aeroelasticity; UAV; Joined Wing; SensorCraft; Flight Test; Unmanned Aircraft

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APA (6th Edition):

Richards, J. (2014). An Experimental Investigation of a Joined Wing Aircraft Configuration Using Flexible, Reduced Scale Flight Test Vehicles. (Thesis). University of Victoria. Retrieved from http://hdl.handle.net/1828/5710

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):

Richards, Jenner. “An Experimental Investigation of a Joined Wing Aircraft Configuration Using Flexible, Reduced Scale Flight Test Vehicles.” 2014. Thesis, University of Victoria. Accessed April 22, 2019. http://hdl.handle.net/1828/5710.

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

MLA Handbook (7th Edition):

Richards, Jenner. “An Experimental Investigation of a Joined Wing Aircraft Configuration Using Flexible, Reduced Scale Flight Test Vehicles.” 2014. Web. 22 Apr 2019.

Vancouver:

Richards J. An Experimental Investigation of a Joined Wing Aircraft Configuration Using Flexible, Reduced Scale Flight Test Vehicles. [Internet] [Thesis]. University of Victoria; 2014. [cited 2019 Apr 22]. Available from: http://hdl.handle.net/1828/5710.

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

Council of Science Editors:

Richards J. An Experimental Investigation of a Joined Wing Aircraft Configuration Using Flexible, Reduced Scale Flight Test Vehicles. [Thesis]. University of Victoria; 2014. Available from: http://hdl.handle.net/1828/5710

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

14. Batalha, Carlos. Da edificação de capacidades militares.

Degree: 2014, IUM

 Findo o bloco soviético e, com ele, desvanecido o inimigo dos Estados ocidentais e a ameaça militar que dele advinha, o conceito de segurança alarga-se… (more)

Subjects/Keywords: Capacidades militares; Segurança Nacional; Dissuasão; Unmanned Aircraft Systems; Sensores; Sistemas complexos

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APA (6th Edition):

Batalha, C. (2014). Da edificação de capacidades militares. (Thesis). IUM. Retrieved from https://www.rcaap.pt/detail.jsp?id=oai:comum.rcaap.pt:10400.26/11392

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):

Batalha, Carlos. “Da edificação de capacidades militares.” 2014. Thesis, IUM. Accessed April 22, 2019. https://www.rcaap.pt/detail.jsp?id=oai:comum.rcaap.pt:10400.26/11392.

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

MLA Handbook (7th Edition):

Batalha, Carlos. “Da edificação de capacidades militares.” 2014. Web. 22 Apr 2019.

Vancouver:

Batalha C. Da edificação de capacidades militares. [Internet] [Thesis]. IUM; 2014. [cited 2019 Apr 22]. Available from: https://www.rcaap.pt/detail.jsp?id=oai:comum.rcaap.pt:10400.26/11392.

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

Council of Science Editors:

Batalha C. Da edificação de capacidades militares. [Thesis]. IUM; 2014. Available from: https://www.rcaap.pt/detail.jsp?id=oai:comum.rcaap.pt:10400.26/11392

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

15. Oliveira, José. O Programa de Sistemas Aéreos Não Tripulados da Força Aérea Portuguesa como alicerce da Capacidade Aérea Não Tripulada Nacional.

Degree: 2014, IUM

 O Programa de Unmanned Aircraft Systems (UAS) da Força Aérea Portuguesa (FAP) tem a sua origem nos trabalhos académicos de investigação realizados na Academia da… (more)

Subjects/Keywords: PITVANT; Unmanned Aircraft System; Capacidade UAS nacional; BTID; Força Aérea Portuguesa

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APA (6th Edition):

Oliveira, J. (2014). O Programa de Sistemas Aéreos Não Tripulados da Força Aérea Portuguesa como alicerce da Capacidade Aérea Não Tripulada Nacional. (Thesis). IUM. Retrieved from https://www.rcaap.pt/detail.jsp?id=oai:comum.rcaap.pt:10400.26/11395

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):

Oliveira, José. “O Programa de Sistemas Aéreos Não Tripulados da Força Aérea Portuguesa como alicerce da Capacidade Aérea Não Tripulada Nacional.” 2014. Thesis, IUM. Accessed April 22, 2019. https://www.rcaap.pt/detail.jsp?id=oai:comum.rcaap.pt:10400.26/11395.

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

MLA Handbook (7th Edition):

Oliveira, José. “O Programa de Sistemas Aéreos Não Tripulados da Força Aérea Portuguesa como alicerce da Capacidade Aérea Não Tripulada Nacional.” 2014. Web. 22 Apr 2019.

Vancouver:

Oliveira J. O Programa de Sistemas Aéreos Não Tripulados da Força Aérea Portuguesa como alicerce da Capacidade Aérea Não Tripulada Nacional. [Internet] [Thesis]. IUM; 2014. [cited 2019 Apr 22]. Available from: https://www.rcaap.pt/detail.jsp?id=oai:comum.rcaap.pt:10400.26/11395.

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

Council of Science Editors:

Oliveira J. O Programa de Sistemas Aéreos Não Tripulados da Força Aérea Portuguesa como alicerce da Capacidade Aérea Não Tripulada Nacional. [Thesis]. IUM; 2014. Available from: https://www.rcaap.pt/detail.jsp?id=oai:comum.rcaap.pt:10400.26/11395

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


Universitat Politècnica de Catalunya

16. Santamaría Barnadas, Eduard. Formal mission specification and execution mechanisms for unmanned aircraft systems.

Degree: Departament d'Arquitectura de Computadors, 2010, Universitat Politècnica de Catalunya

Unmanned Aircraft Systems (UAS) are rapidly gaining attention due to the increasing potential of their applications in the civil domain. UAS can provide great value… (more)

Subjects/Keywords: flight management; mission management; unmanned aircraft systems; UAS; 004

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APA (6th Edition):

Santamaría Barnadas, E. (2010). Formal mission specification and execution mechanisms for unmanned aircraft systems. (Thesis). Universitat Politècnica de Catalunya. Retrieved from http://hdl.handle.net/10803/6020

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):

Santamaría Barnadas, Eduard. “Formal mission specification and execution mechanisms for unmanned aircraft systems.” 2010. Thesis, Universitat Politècnica de Catalunya. Accessed April 22, 2019. http://hdl.handle.net/10803/6020.

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

MLA Handbook (7th Edition):

Santamaría Barnadas, Eduard. “Formal mission specification and execution mechanisms for unmanned aircraft systems.” 2010. Web. 22 Apr 2019.

Vancouver:

Santamaría Barnadas E. Formal mission specification and execution mechanisms for unmanned aircraft systems. [Internet] [Thesis]. Universitat Politècnica de Catalunya; 2010. [cited 2019 Apr 22]. Available from: http://hdl.handle.net/10803/6020.

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

Council of Science Editors:

Santamaría Barnadas E. Formal mission specification and execution mechanisms for unmanned aircraft systems. [Thesis]. Universitat Politècnica de Catalunya; 2010. Available from: http://hdl.handle.net/10803/6020

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


Universidade Nova

17. Jordán, Emilio Troncho. A prospective geoinformatic approach to indoor navigation for Unmanned Air System (UAS) by use of quick response (QR) codes.

Degree: 2016, Universidade Nova

 This research study explores a navigation system for autonomous indoor flight of Unmanned Aircraft Systems (UAS) dead reckoning with Inertial Navigation System (INS) and the… (more)

Subjects/Keywords: Unmanned Aircraft System; Indoor Navigation; QR codes; Inertial Navigation System

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APA (6th Edition):

Jordán, E. T. (2016). A prospective geoinformatic approach to indoor navigation for Unmanned Air System (UAS) by use of quick response (QR) codes. (Thesis). Universidade Nova. Retrieved from http://www.rcaap.pt/detail.jsp?id=oai:run.unl.pt:10362/18406

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):

Jordán, Emilio Troncho. “A prospective geoinformatic approach to indoor navigation for Unmanned Air System (UAS) by use of quick response (QR) codes.” 2016. Thesis, Universidade Nova. Accessed April 22, 2019. http://www.rcaap.pt/detail.jsp?id=oai:run.unl.pt:10362/18406.

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

MLA Handbook (7th Edition):

Jordán, Emilio Troncho. “A prospective geoinformatic approach to indoor navigation for Unmanned Air System (UAS) by use of quick response (QR) codes.” 2016. Web. 22 Apr 2019.

Vancouver:

Jordán ET. A prospective geoinformatic approach to indoor navigation for Unmanned Air System (UAS) by use of quick response (QR) codes. [Internet] [Thesis]. Universidade Nova; 2016. [cited 2019 Apr 22]. Available from: http://www.rcaap.pt/detail.jsp?id=oai:run.unl.pt:10362/18406.

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

Council of Science Editors:

Jordán ET. A prospective geoinformatic approach to indoor navigation for Unmanned Air System (UAS) by use of quick response (QR) codes. [Thesis]. Universidade Nova; 2016. Available from: http://www.rcaap.pt/detail.jsp?id=oai:run.unl.pt:10362/18406

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


Mississippi State University

18. Edwards, Christopher Doyle. NONLINEAR SIX DEGREE-OF-FREEDOM SIMULATOR FOR A SMALL UNMANNED AERIAL VEHICLE.

Degree: MS, Electrical and Computer Engineering, 2010, Mississippi State University

Aircraft modeling and simulation have become increasingly important in the areas of pilot training, safety and aircraft design, especially for unmanned aerial vehicles (UAVs). A… (more)

Subjects/Keywords: aircraft; simulator; MATLAB; Simulink; unmanned aerial vehicle; UAV; Xipiter; FlightGear

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APA (6th Edition):

Edwards, C. D. (2010). NONLINEAR SIX DEGREE-OF-FREEDOM SIMULATOR FOR A SMALL UNMANNED AERIAL VEHICLE. (Masters Thesis). Mississippi State University. Retrieved from http://sun.library.msstate.edu/ETD-db/theses/available/etd-03312010-125540/ ;

Chicago Manual of Style (16th Edition):

Edwards, Christopher Doyle. “NONLINEAR SIX DEGREE-OF-FREEDOM SIMULATOR FOR A SMALL UNMANNED AERIAL VEHICLE.” 2010. Masters Thesis, Mississippi State University. Accessed April 22, 2019. http://sun.library.msstate.edu/ETD-db/theses/available/etd-03312010-125540/ ;.

MLA Handbook (7th Edition):

Edwards, Christopher Doyle. “NONLINEAR SIX DEGREE-OF-FREEDOM SIMULATOR FOR A SMALL UNMANNED AERIAL VEHICLE.” 2010. Web. 22 Apr 2019.

Vancouver:

Edwards CD. NONLINEAR SIX DEGREE-OF-FREEDOM SIMULATOR FOR A SMALL UNMANNED AERIAL VEHICLE. [Internet] [Masters thesis]. Mississippi State University; 2010. [cited 2019 Apr 22]. Available from: http://sun.library.msstate.edu/ETD-db/theses/available/etd-03312010-125540/ ;.

Council of Science Editors:

Edwards CD. NONLINEAR SIX DEGREE-OF-FREEDOM SIMULATOR FOR A SMALL UNMANNED AERIAL VEHICLE. [Masters Thesis]. Mississippi State University; 2010. Available from: http://sun.library.msstate.edu/ETD-db/theses/available/etd-03312010-125540/ ;


Georgia Tech

19. Kim, Sungjin. User-perceived effectiveness of unmanned aircraft system (UAS) integration in infrastructure construction environments.

Degree: PhD, Building Construction, 2018, Georgia Tech

 A multi-layered performance analysis (MPA) method was proposed. Information analysis, technology performance, and human performance addressed based on the users' experience and perception measurement method… (more)

Subjects/Keywords: Unmanned aircraft system (UAS) in construction; Multi-layered performance analysis

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APA (6th Edition):

Kim, S. (2018). User-perceived effectiveness of unmanned aircraft system (UAS) integration in infrastructure construction environments. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/59899

Chicago Manual of Style (16th Edition):

Kim, Sungjin. “User-perceived effectiveness of unmanned aircraft system (UAS) integration in infrastructure construction environments.” 2018. Doctoral Dissertation, Georgia Tech. Accessed April 22, 2019. http://hdl.handle.net/1853/59899.

MLA Handbook (7th Edition):

Kim, Sungjin. “User-perceived effectiveness of unmanned aircraft system (UAS) integration in infrastructure construction environments.” 2018. Web. 22 Apr 2019.

Vancouver:

Kim S. User-perceived effectiveness of unmanned aircraft system (UAS) integration in infrastructure construction environments. [Internet] [Doctoral dissertation]. Georgia Tech; 2018. [cited 2019 Apr 22]. Available from: http://hdl.handle.net/1853/59899.

Council of Science Editors:

Kim S. User-perceived effectiveness of unmanned aircraft system (UAS) integration in infrastructure construction environments. [Doctoral Dissertation]. Georgia Tech; 2018. Available from: http://hdl.handle.net/1853/59899


University of Michigan

20. Jones, Jessica. Development of a Very Flexible Testbed Aircraft for the Validation of Nonlinear Aeroelastic Codes.

Degree: PhD, Aerospace Engineering, 2017, University of Michigan

 This dissertation presents the development, analysis, and flight testing of an unmanned aeroelastic testbed aircraft. The experimental, remotely-piloted aircraft was designed to be aeroelastically representative… (more)

Subjects/Keywords: aeroelasticity; flight testing; unmanned aircraft; nonlinear simulation; Aerospace Engineering; Engineering

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

APA (6th Edition):

Jones, J. (2017). Development of a Very Flexible Testbed Aircraft for the Validation of Nonlinear Aeroelastic Codes. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/140822

Chicago Manual of Style (16th Edition):

Jones, Jessica. “Development of a Very Flexible Testbed Aircraft for the Validation of Nonlinear Aeroelastic Codes.” 2017. Doctoral Dissertation, University of Michigan. Accessed April 22, 2019. http://hdl.handle.net/2027.42/140822.

MLA Handbook (7th Edition):

Jones, Jessica. “Development of a Very Flexible Testbed Aircraft for the Validation of Nonlinear Aeroelastic Codes.” 2017. Web. 22 Apr 2019.

Vancouver:

Jones J. Development of a Very Flexible Testbed Aircraft for the Validation of Nonlinear Aeroelastic Codes. [Internet] [Doctoral dissertation]. University of Michigan; 2017. [cited 2019 Apr 22]. Available from: http://hdl.handle.net/2027.42/140822.

Council of Science Editors:

Jones J. Development of a Very Flexible Testbed Aircraft for the Validation of Nonlinear Aeroelastic Codes. [Doctoral Dissertation]. University of Michigan; 2017. Available from: http://hdl.handle.net/2027.42/140822


Virginia Tech

21. Aarons, Tyler David. Development and Implementation of a Flight Test Program for a Geometrically Scaled Joined Wing SensorCraft Remotely Piloted Vehicle.

Degree: MS, Aerospace and Ocean Engineering, 2011, Virginia Tech

 The development and implementation of a flight test program for an unmanned aircraft is a multidisciplinary challenge. This thesis presents the development and implementation of… (more)

Subjects/Keywords: Flight Test; SensorCraft; Joined Wing; RPV; Remotely Piloted Vehicle; Scaling; UAS; UAV; Unmanned Aerial Vehicle; Unmanned Aircraft

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

APA (6th Edition):

Aarons, T. D. (2011). Development and Implementation of a Flight Test Program for a Geometrically Scaled Joined Wing SensorCraft Remotely Piloted Vehicle. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/36383

Chicago Manual of Style (16th Edition):

Aarons, Tyler David. “Development and Implementation of a Flight Test Program for a Geometrically Scaled Joined Wing SensorCraft Remotely Piloted Vehicle.” 2011. Masters Thesis, Virginia Tech. Accessed April 22, 2019. http://hdl.handle.net/10919/36383.

MLA Handbook (7th Edition):

Aarons, Tyler David. “Development and Implementation of a Flight Test Program for a Geometrically Scaled Joined Wing SensorCraft Remotely Piloted Vehicle.” 2011. Web. 22 Apr 2019.

Vancouver:

Aarons TD. Development and Implementation of a Flight Test Program for a Geometrically Scaled Joined Wing SensorCraft Remotely Piloted Vehicle. [Internet] [Masters thesis]. Virginia Tech; 2011. [cited 2019 Apr 22]. Available from: http://hdl.handle.net/10919/36383.

Council of Science Editors:

Aarons TD. Development and Implementation of a Flight Test Program for a Geometrically Scaled Joined Wing SensorCraft Remotely Piloted Vehicle. [Masters Thesis]. Virginia Tech; 2011. Available from: http://hdl.handle.net/10919/36383


Virginia Tech

22. Garnand-Royo, Jeffrey Samuel. Design and Evaluation of Geometric Nonlinearities using Joined-Wing SensorCraft Flight Test Article.

Degree: MS, Aerospace and Ocean Engineering, 2013, Virginia Tech

 The Boeing Joined-Wing SenorCraft is a novel aircraft design that has many potential benefits, especially for surveillance missions. However, computational studies have shown the potential… (more)

Subjects/Keywords: oined Wing; SensorCraft; Flight Test; Unmanned Aircraft; Unmanned Aerial Vehicle; UAV; UAS; Scaling; Remotely Piloted Vehicle; R

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APA (6th Edition):

Garnand-Royo, J. S. (2013). Design and Evaluation of Geometric Nonlinearities using Joined-Wing SensorCraft Flight Test Article. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/23234

Chicago Manual of Style (16th Edition):

Garnand-Royo, Jeffrey Samuel. “Design and Evaluation of Geometric Nonlinearities using Joined-Wing SensorCraft Flight Test Article.” 2013. Masters Thesis, Virginia Tech. Accessed April 22, 2019. http://hdl.handle.net/10919/23234.

MLA Handbook (7th Edition):

Garnand-Royo, Jeffrey Samuel. “Design and Evaluation of Geometric Nonlinearities using Joined-Wing SensorCraft Flight Test Article.” 2013. Web. 22 Apr 2019.

Vancouver:

Garnand-Royo JS. Design and Evaluation of Geometric Nonlinearities using Joined-Wing SensorCraft Flight Test Article. [Internet] [Masters thesis]. Virginia Tech; 2013. [cited 2019 Apr 22]. Available from: http://hdl.handle.net/10919/23234.

Council of Science Editors:

Garnand-Royo JS. Design and Evaluation of Geometric Nonlinearities using Joined-Wing SensorCraft Flight Test Article. [Masters Thesis]. Virginia Tech; 2013. Available from: http://hdl.handle.net/10919/23234


University of Kentucky

23. McCray, Robert B. UTILIZATION OF A SMALL UNMANNED AIRCRAFT SYSTEM FOR DIRECT SAMPLING OF NITROGEN OXIDES PRODUCED BY FULL-SCALE SURFACE MINE BLASTING.

Degree: 2016, University of Kentucky

 Emerging health concern for gaseous nitrogen oxides (NOx) emitted during surface mine blasting has prompted mining authorities in the United States to pursue new regulations.… (more)

Subjects/Keywords: Nitrogen Oxides; Explosive Gases; Surface Mine Blasting; Small Unmanned Aircraft System; Gas Monitoring; Mining Engineering

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APA (6th Edition):

McCray, R. B. (2016). UTILIZATION OF A SMALL UNMANNED AIRCRAFT SYSTEM FOR DIRECT SAMPLING OF NITROGEN OXIDES PRODUCED BY FULL-SCALE SURFACE MINE BLASTING. (Masters Thesis). University of Kentucky. Retrieved from http://uknowledge.uky.edu/mng_etds/31

Chicago Manual of Style (16th Edition):

McCray, Robert B. “UTILIZATION OF A SMALL UNMANNED AIRCRAFT SYSTEM FOR DIRECT SAMPLING OF NITROGEN OXIDES PRODUCED BY FULL-SCALE SURFACE MINE BLASTING.” 2016. Masters Thesis, University of Kentucky. Accessed April 22, 2019. http://uknowledge.uky.edu/mng_etds/31.

MLA Handbook (7th Edition):

McCray, Robert B. “UTILIZATION OF A SMALL UNMANNED AIRCRAFT SYSTEM FOR DIRECT SAMPLING OF NITROGEN OXIDES PRODUCED BY FULL-SCALE SURFACE MINE BLASTING.” 2016. Web. 22 Apr 2019.

Vancouver:

McCray RB. UTILIZATION OF A SMALL UNMANNED AIRCRAFT SYSTEM FOR DIRECT SAMPLING OF NITROGEN OXIDES PRODUCED BY FULL-SCALE SURFACE MINE BLASTING. [Internet] [Masters thesis]. University of Kentucky; 2016. [cited 2019 Apr 22]. Available from: http://uknowledge.uky.edu/mng_etds/31.

Council of Science Editors:

McCray RB. UTILIZATION OF A SMALL UNMANNED AIRCRAFT SYSTEM FOR DIRECT SAMPLING OF NITROGEN OXIDES PRODUCED BY FULL-SCALE SURFACE MINE BLASTING. [Masters Thesis]. University of Kentucky; 2016. Available from: http://uknowledge.uky.edu/mng_etds/31


University of Colorado

24. Shaw-Cortez, Wenceslao Eric. Energy-Aware Path Planning for UAS Persistent Sampling and Surveillance.

Degree: MS, Aerospace Engineering Sciences, 2013, University of Colorado

  The focus of this work is to develop an energy-aware path planning algorithm that maximizes UAS endurance, while performing sampling and surveillance missions in… (more)

Subjects/Keywords: Control Systems; Optimization; Path Planning in Wind; Unmanned Aircraft Systems; Aerospace Engineering; Propulsion and Power

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APA (6th Edition):

Shaw-Cortez, W. E. (2013). Energy-Aware Path Planning for UAS Persistent Sampling and Surveillance. (Masters Thesis). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/76

Chicago Manual of Style (16th Edition):

Shaw-Cortez, Wenceslao Eric. “Energy-Aware Path Planning for UAS Persistent Sampling and Surveillance.” 2013. Masters Thesis, University of Colorado. Accessed April 22, 2019. http://scholar.colorado.edu/asen_gradetds/76.

MLA Handbook (7th Edition):

Shaw-Cortez, Wenceslao Eric. “Energy-Aware Path Planning for UAS Persistent Sampling and Surveillance.” 2013. Web. 22 Apr 2019.

Vancouver:

Shaw-Cortez WE. Energy-Aware Path Planning for UAS Persistent Sampling and Surveillance. [Internet] [Masters thesis]. University of Colorado; 2013. [cited 2019 Apr 22]. Available from: http://scholar.colorado.edu/asen_gradetds/76.

Council of Science Editors:

Shaw-Cortez WE. Energy-Aware Path Planning for UAS Persistent Sampling and Surveillance. [Masters Thesis]. University of Colorado; 2013. Available from: http://scholar.colorado.edu/asen_gradetds/76


Georgia Tech

25. Tangen, Steven Anthony. A methodology for the quantification of doctrine and materiel approaches in a capability-based assessment.

Degree: PhD, Aerospace Engineering, 2009, Georgia Tech

 Due to the complexities of modern military operations and the technologies employed on today's military systems, acquisition costs and development times are becoming increasingly large.… (more)

Subjects/Keywords: Aerospace engineering; Doctrine; JCIDS; Unmanned aircraft; Defense acquisition; Operational readiness (Military science) Analysis; Technology Design

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APA (6th Edition):

Tangen, S. A. (2009). A methodology for the quantification of doctrine and materiel approaches in a capability-based assessment. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/28105

Chicago Manual of Style (16th Edition):

Tangen, Steven Anthony. “A methodology for the quantification of doctrine and materiel approaches in a capability-based assessment.” 2009. Doctoral Dissertation, Georgia Tech. Accessed April 22, 2019. http://hdl.handle.net/1853/28105.

MLA Handbook (7th Edition):

Tangen, Steven Anthony. “A methodology for the quantification of doctrine and materiel approaches in a capability-based assessment.” 2009. Web. 22 Apr 2019.

Vancouver:

Tangen SA. A methodology for the quantification of doctrine and materiel approaches in a capability-based assessment. [Internet] [Doctoral dissertation]. Georgia Tech; 2009. [cited 2019 Apr 22]. Available from: http://hdl.handle.net/1853/28105.

Council of Science Editors:

Tangen SA. A methodology for the quantification of doctrine and materiel approaches in a capability-based assessment. [Doctoral Dissertation]. Georgia Tech; 2009. Available from: http://hdl.handle.net/1853/28105


University of Southern California

26. Parker, Mary Elizabeth. Data overload in unmanned aircraft systems: improving bandwidth utilization through wavelet compression.

Degree: MS, Geographic Information Science and Technology, 2013, University of Southern California

 Between 2008 and 2010, the number of unmanned aircraft systems (UAS) in the military increased by 330% in support of operations throughout the Middle East… (more)

Subjects/Keywords: military; UAS; unmanned aircraft; image compression; wavelet compression; ECW; tactical; bandwidth utilization

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APA (6th Edition):

Parker, M. E. (2013). Data overload in unmanned aircraft systems: improving bandwidth utilization through wavelet compression. (Masters Thesis). University of Southern California. Retrieved from http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/243817/rec/1765

Chicago Manual of Style (16th Edition):

Parker, Mary Elizabeth. “Data overload in unmanned aircraft systems: improving bandwidth utilization through wavelet compression.” 2013. Masters Thesis, University of Southern California. Accessed April 22, 2019. http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/243817/rec/1765.

MLA Handbook (7th Edition):

Parker, Mary Elizabeth. “Data overload in unmanned aircraft systems: improving bandwidth utilization through wavelet compression.” 2013. Web. 22 Apr 2019.

Vancouver:

Parker ME. Data overload in unmanned aircraft systems: improving bandwidth utilization through wavelet compression. [Internet] [Masters thesis]. University of Southern California; 2013. [cited 2019 Apr 22]. Available from: http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/243817/rec/1765.

Council of Science Editors:

Parker ME. Data overload in unmanned aircraft systems: improving bandwidth utilization through wavelet compression. [Masters Thesis]. University of Southern California; 2013. Available from: http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/243817/rec/1765

27. Chiote, Diogo. Requisitos Operacionais para os Veículos Aéreos Não Tripulados (UAV) na Guarda Nacional Republicana.

Degree: 2012, Academia Militar. Direção de Ensino

O desenvolvimento tecnológico na área da aviação autónoma, nomeadamente nos Veículos Aéreos Não Tripulados, revela características que poderão ser utilizadas pela Guarda Nacional Republicana no… (more)

Subjects/Keywords: Guarda Nacional Republicana; Veículos Aéreos Não Tripulados; Requisitos Operacionais; Unmanned Aircraft System

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

APA (6th Edition):

Chiote, D. (2012). Requisitos Operacionais para os Veículos Aéreos Não Tripulados (UAV) na Guarda Nacional Republicana. (Thesis). Academia Militar. Direção de Ensino. Retrieved from https://www.rcaap.pt/detail.jsp?id=oai:comum.rcaap.pt:10400.26/8534

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):

Chiote, Diogo. “Requisitos Operacionais para os Veículos Aéreos Não Tripulados (UAV) na Guarda Nacional Republicana.” 2012. Thesis, Academia Militar. Direção de Ensino. Accessed April 22, 2019. https://www.rcaap.pt/detail.jsp?id=oai:comum.rcaap.pt:10400.26/8534.

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

MLA Handbook (7th Edition):

Chiote, Diogo. “Requisitos Operacionais para os Veículos Aéreos Não Tripulados (UAV) na Guarda Nacional Republicana.” 2012. Web. 22 Apr 2019.

Vancouver:

Chiote D. Requisitos Operacionais para os Veículos Aéreos Não Tripulados (UAV) na Guarda Nacional Republicana. [Internet] [Thesis]. Academia Militar. Direção de Ensino; 2012. [cited 2019 Apr 22]. Available from: https://www.rcaap.pt/detail.jsp?id=oai:comum.rcaap.pt:10400.26/8534.

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

Council of Science Editors:

Chiote D. Requisitos Operacionais para os Veículos Aéreos Não Tripulados (UAV) na Guarda Nacional Republicana. [Thesis]. Academia Militar. Direção de Ensino; 2012. Available from: https://www.rcaap.pt/detail.jsp?id=oai:comum.rcaap.pt:10400.26/8534

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


Queensland University of Technology

28. Clothier, Reece Alexander. Decision support for the safe design and operation of unmanned aircraft systems.

Degree: 2012, Queensland University of Technology

Unmanned Aircraft Systems (UAS) describe a diverse range of aircraft that are operated without a human pilot on-board. Unmanned aircraft range from small rotorcraft, which… (more)

Subjects/Keywords: safety; risk; decision; support; theory; systems; philosophy; UAS; UAV; unmanned; aircraft; systems; regulation

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

APA (6th Edition):

Clothier, R. A. (2012). Decision support for the safe design and operation of unmanned aircraft systems. (Thesis). Queensland University of Technology. Retrieved from https://eprints.qut.edu.au/51048/

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):

Clothier, Reece Alexander. “Decision support for the safe design and operation of unmanned aircraft systems.” 2012. Thesis, Queensland University of Technology. Accessed April 22, 2019. https://eprints.qut.edu.au/51048/.

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

MLA Handbook (7th Edition):

Clothier, Reece Alexander. “Decision support for the safe design and operation of unmanned aircraft systems.” 2012. Web. 22 Apr 2019.

Vancouver:

Clothier RA. Decision support for the safe design and operation of unmanned aircraft systems. [Internet] [Thesis]. Queensland University of Technology; 2012. [cited 2019 Apr 22]. Available from: https://eprints.qut.edu.au/51048/.

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

Council of Science Editors:

Clothier RA. Decision support for the safe design and operation of unmanned aircraft systems. [Thesis]. Queensland University of Technology; 2012. Available from: https://eprints.qut.edu.au/51048/

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


Delft University of Technology

29. Spirlet, G.B. Design of Morphing Leading and Trailing Edge Surfaces for Camber and Twist Control:.

Degree: 2015, Delft University of Technology

 The application of morphing structures in conventional aircraft is a method to improve aircraft performance by both reducing the total fuel consumption for a given… (more)

Subjects/Keywords: morphing; morhping; uav; unmanned; aircraft; twist; camber; flap; aileron; adaptive; high lift device; variable

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

APA (6th Edition):

Spirlet, G. B. (2015). Design of Morphing Leading and Trailing Edge Surfaces for Camber and Twist Control:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:241ef267-13e7-4e6f-902e-202d0b15b58f

Chicago Manual of Style (16th Edition):

Spirlet, G B. “Design of Morphing Leading and Trailing Edge Surfaces for Camber and Twist Control:.” 2015. Masters Thesis, Delft University of Technology. Accessed April 22, 2019. http://resolver.tudelft.nl/uuid:241ef267-13e7-4e6f-902e-202d0b15b58f.

MLA Handbook (7th Edition):

Spirlet, G B. “Design of Morphing Leading and Trailing Edge Surfaces for Camber and Twist Control:.” 2015. Web. 22 Apr 2019.

Vancouver:

Spirlet GB. Design of Morphing Leading and Trailing Edge Surfaces for Camber and Twist Control:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2019 Apr 22]. Available from: http://resolver.tudelft.nl/uuid:241ef267-13e7-4e6f-902e-202d0b15b58f.

Council of Science Editors:

Spirlet GB. Design of Morphing Leading and Trailing Edge Surfaces for Camber and Twist Control:. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:241ef267-13e7-4e6f-902e-202d0b15b58f


Brno University of Technology

30. Mocek, Jurij. Létající robot pro geofyzikální účely .

Degree: 2013, Brno University of Technology

 Cílem této práce je navrhnout konstrukční řešení pro dálkově řízený létající stroj s důrazem na svislý start, vznášení se na jednom místě a svislé přistání.… (more)

Subjects/Keywords: Létající robot; bezpilotní letoun; měření tahu; multikoptéra; Flying robot; unmanned aircraft; measurement of thrust; multicopter

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

APA (6th Edition):

Mocek, J. (2013). Létající robot pro geofyzikální účely . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/25509

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):

Mocek, Jurij. “Létající robot pro geofyzikální účely .” 2013. Thesis, Brno University of Technology. Accessed April 22, 2019. http://hdl.handle.net/11012/25509.

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

MLA Handbook (7th Edition):

Mocek, Jurij. “Létající robot pro geofyzikální účely .” 2013. Web. 22 Apr 2019.

Vancouver:

Mocek J. Létající robot pro geofyzikální účely . [Internet] [Thesis]. Brno University of Technology; 2013. [cited 2019 Apr 22]. Available from: http://hdl.handle.net/11012/25509.

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

Council of Science Editors:

Mocek J. Létající robot pro geofyzikální účely . [Thesis]. Brno University of Technology; 2013. Available from: http://hdl.handle.net/11012/25509

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

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