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You searched for subject:(Landing aids Aeronautics ). Showing records 1 – 30 of 11216 total matches.

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Stellenbosch University

1. Mfiri, Tatenda Joshua. Autonomous landing of a tethered multi-rotor unmanned aerial vehicle on a stationary platform.

Degree: MScEng, Electrical and Electronic Engineering, 2019, Stellenbosch University

ENGLISH ABSTRACT: This thesis contributes to the research of persistent tethered aerial vehicles by presenting a strategy to autonomously land a tethered multi-rotor UAV. A… (more)

Subjects/Keywords: Landing aids (Aeronautics); Tethered space vehicles; Unmanned aerial vehicles; UCTD

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APA (6th Edition):

Mfiri, T. J. (2019). Autonomous landing of a tethered multi-rotor unmanned aerial vehicle on a stationary platform. (Masters Thesis). Stellenbosch University. Retrieved from http://hdl.handle.net/10019.1/105897

Chicago Manual of Style (16th Edition):

Mfiri, Tatenda Joshua. “Autonomous landing of a tethered multi-rotor unmanned aerial vehicle on a stationary platform.” 2019. Masters Thesis, Stellenbosch University. Accessed January 17, 2020. http://hdl.handle.net/10019.1/105897.

MLA Handbook (7th Edition):

Mfiri, Tatenda Joshua. “Autonomous landing of a tethered multi-rotor unmanned aerial vehicle on a stationary platform.” 2019. Web. 17 Jan 2020.

Vancouver:

Mfiri TJ. Autonomous landing of a tethered multi-rotor unmanned aerial vehicle on a stationary platform. [Internet] [Masters thesis]. Stellenbosch University; 2019. [cited 2020 Jan 17]. Available from: http://hdl.handle.net/10019.1/105897.

Council of Science Editors:

Mfiri TJ. Autonomous landing of a tethered multi-rotor unmanned aerial vehicle on a stationary platform. [Masters Thesis]. Stellenbosch University; 2019. Available from: http://hdl.handle.net/10019.1/105897


University of Oklahoma

2. Huang, Yih-Ru. OPTOELECTRONIC THREE-DIMENSIONAL TRACKING SYSTEM FOR COLLISION RISK MODEL.

Degree: PhD, 2009, University of Oklahoma

 The CRM system is new and novel concept and is the first successful low cost attempt to visually track a high speed approaching aircraft. The… (more)

Subjects/Keywords: Airplanes – Collision avoidance; Landing aids (Aeronautics); Instrument landing systems

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APA (6th Edition):

Huang, Y. (2009). OPTOELECTRONIC THREE-DIMENSIONAL TRACKING SYSTEM FOR COLLISION RISK MODEL. (Doctoral Dissertation). University of Oklahoma. Retrieved from http://hdl.handle.net/11244/319318

Chicago Manual of Style (16th Edition):

Huang, Yih-Ru. “OPTOELECTRONIC THREE-DIMENSIONAL TRACKING SYSTEM FOR COLLISION RISK MODEL.” 2009. Doctoral Dissertation, University of Oklahoma. Accessed January 17, 2020. http://hdl.handle.net/11244/319318.

MLA Handbook (7th Edition):

Huang, Yih-Ru. “OPTOELECTRONIC THREE-DIMENSIONAL TRACKING SYSTEM FOR COLLISION RISK MODEL.” 2009. Web. 17 Jan 2020.

Vancouver:

Huang Y. OPTOELECTRONIC THREE-DIMENSIONAL TRACKING SYSTEM FOR COLLISION RISK MODEL. [Internet] [Doctoral dissertation]. University of Oklahoma; 2009. [cited 2020 Jan 17]. Available from: http://hdl.handle.net/11244/319318.

Council of Science Editors:

Huang Y. OPTOELECTRONIC THREE-DIMENSIONAL TRACKING SYSTEM FOR COLLISION RISK MODEL. [Doctoral Dissertation]. University of Oklahoma; 2009. Available from: http://hdl.handle.net/11244/319318


Virginia Tech

3. Haile, James Ernest. An analysis of the static and dynamic characteristics of a decoupled landing entry vehicle.

Degree: MS, Aerospace Engineering, 1968, Virginia Tech

Subjects/Keywords: LD5655.V855 1968.H32; Landing aids (Aeronautics)

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APA (6th Edition):

Haile, J. E. (1968). An analysis of the static and dynamic characteristics of a decoupled landing entry vehicle. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/64581

Chicago Manual of Style (16th Edition):

Haile, James Ernest. “An analysis of the static and dynamic characteristics of a decoupled landing entry vehicle.” 1968. Masters Thesis, Virginia Tech. Accessed January 17, 2020. http://hdl.handle.net/10919/64581.

MLA Handbook (7th Edition):

Haile, James Ernest. “An analysis of the static and dynamic characteristics of a decoupled landing entry vehicle.” 1968. Web. 17 Jan 2020.

Vancouver:

Haile JE. An analysis of the static and dynamic characteristics of a decoupled landing entry vehicle. [Internet] [Masters thesis]. Virginia Tech; 1968. [cited 2020 Jan 17]. Available from: http://hdl.handle.net/10919/64581.

Council of Science Editors:

Haile JE. An analysis of the static and dynamic characteristics of a decoupled landing entry vehicle. [Masters Thesis]. Virginia Tech; 1968. Available from: http://hdl.handle.net/10919/64581

4. Li, Wei, 1982-. Simultaneous variable selection and outlier detection using LASSO with applications to aircraft landing data analysis.

Degree: Statistics and Biostatistics, 2012, Rutgers University

Subjects/Keywords: Instrumental variables (Statistics); Airplanes – Landing; Landing aids (Aeronautics)

…simulation in section 7, we will apply our method to the aircraft landing data analysis in section… 

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

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APA (6th Edition):

Li, Wei, 1. (2012). Simultaneous variable selection and outlier detection using LASSO with applications to aircraft landing data analysis. (Thesis). Rutgers University. Retrieved from http://hdl.rutgers.edu/1782.1/rucore10001600001.ETD.000065195

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):

Li, Wei, 1982-. “Simultaneous variable selection and outlier detection using LASSO with applications to aircraft landing data analysis.” 2012. Thesis, Rutgers University. Accessed January 17, 2020. http://hdl.rutgers.edu/1782.1/rucore10001600001.ETD.000065195.

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

MLA Handbook (7th Edition):

Li, Wei, 1982-. “Simultaneous variable selection and outlier detection using LASSO with applications to aircraft landing data analysis.” 2012. Web. 17 Jan 2020.

Vancouver:

Li, Wei 1. Simultaneous variable selection and outlier detection using LASSO with applications to aircraft landing data analysis. [Internet] [Thesis]. Rutgers University; 2012. [cited 2020 Jan 17]. Available from: http://hdl.rutgers.edu/1782.1/rucore10001600001.ETD.000065195.

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

Council of Science Editors:

Li, Wei 1. Simultaneous variable selection and outlier detection using LASSO with applications to aircraft landing data analysis. [Thesis]. Rutgers University; 2012. Available from: http://hdl.rutgers.edu/1782.1/rucore10001600001.ETD.000065195

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


Texas A&M University

5. Anderson, Thomas Edward. A total energy sensor for glidepath and speed control of a tactical airlifter in wind shear.

Degree: MS, aerospace engineering, 2012, Texas A&M University

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.; Landing aids (Aeronautics) - Mathematical models.; Landing aids (Aeronautics) - Data processing.; Detectors - Testing.; Vertical wind shear.

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APA (6th Edition):

Anderson, T. E. (2012). A total energy sensor for glidepath and speed control of a tactical airlifter in wind shear. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1987-THESIS-A551

Chicago Manual of Style (16th Edition):

Anderson, Thomas Edward. “A total energy sensor for glidepath and speed control of a tactical airlifter in wind shear.” 2012. Masters Thesis, Texas A&M University. Accessed January 17, 2020. http://hdl.handle.net/1969.1/ETD-TAMU-1987-THESIS-A551.

MLA Handbook (7th Edition):

Anderson, Thomas Edward. “A total energy sensor for glidepath and speed control of a tactical airlifter in wind shear.” 2012. Web. 17 Jan 2020.

Vancouver:

Anderson TE. A total energy sensor for glidepath and speed control of a tactical airlifter in wind shear. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2020 Jan 17]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1987-THESIS-A551.

Council of Science Editors:

Anderson TE. A total energy sensor for glidepath and speed control of a tactical airlifter in wind shear. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1987-THESIS-A551


MIT

6. McMuldroch, Christopher Graham. VTOL controls for shipboard landing .

Degree: MS, Aeronautics and Astronautics, 1979, MIT

Subjects/Keywords: Aeronautics and Astronautics.; Vertically rising aircraft; Landing aids (Aeronautics); Ships Seakeeping; Naval aviation

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APA (6th Edition):

McMuldroch, C. G. (1979). VTOL controls for shipboard landing . (Masters Thesis). MIT. Retrieved from http://hdl.handle.net/1721.1/16070

Chicago Manual of Style (16th Edition):

McMuldroch, Christopher Graham. “VTOL controls for shipboard landing .” 1979. Masters Thesis, MIT. Accessed January 17, 2020. http://hdl.handle.net/1721.1/16070.

MLA Handbook (7th Edition):

McMuldroch, Christopher Graham. “VTOL controls for shipboard landing .” 1979. Web. 17 Jan 2020.

Vancouver:

McMuldroch CG. VTOL controls for shipboard landing . [Internet] [Masters thesis]. MIT; 1979. [cited 2020 Jan 17]. Available from: http://hdl.handle.net/1721.1/16070.

Council of Science Editors:

McMuldroch CG. VTOL controls for shipboard landing . [Masters Thesis]. MIT; 1979. Available from: http://hdl.handle.net/1721.1/16070


University of Oklahoma

7. McCartor, Gerry Ray. IDENTIFICATION OF EXTREMELY LOW FREQUENCY ERROR COMPONENTS IN THE GLOBAL POSITIONING SYSTEM (GPS)/WIDE AREA AUGMENTATION SYSTEM (WAAS) POSITION SOLUTION.

Degree: PhD, 2009, University of Oklahoma

 Means of applying corrections for these errors are presented as well as areas of future research and investigation. If the corrections identified by this dissertation… (more)

Subjects/Keywords: Instrument landing systems; Navigation (Aeronautics); Air traffic control; Global Positioning System; Landing aids (Aeronautics)

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APA (6th Edition):

McCartor, G. R. (2009). IDENTIFICATION OF EXTREMELY LOW FREQUENCY ERROR COMPONENTS IN THE GLOBAL POSITIONING SYSTEM (GPS)/WIDE AREA AUGMENTATION SYSTEM (WAAS) POSITION SOLUTION. (Doctoral Dissertation). University of Oklahoma. Retrieved from http://hdl.handle.net/11244/320318

Chicago Manual of Style (16th Edition):

McCartor, Gerry Ray. “IDENTIFICATION OF EXTREMELY LOW FREQUENCY ERROR COMPONENTS IN THE GLOBAL POSITIONING SYSTEM (GPS)/WIDE AREA AUGMENTATION SYSTEM (WAAS) POSITION SOLUTION.” 2009. Doctoral Dissertation, University of Oklahoma. Accessed January 17, 2020. http://hdl.handle.net/11244/320318.

MLA Handbook (7th Edition):

McCartor, Gerry Ray. “IDENTIFICATION OF EXTREMELY LOW FREQUENCY ERROR COMPONENTS IN THE GLOBAL POSITIONING SYSTEM (GPS)/WIDE AREA AUGMENTATION SYSTEM (WAAS) POSITION SOLUTION.” 2009. Web. 17 Jan 2020.

Vancouver:

McCartor GR. IDENTIFICATION OF EXTREMELY LOW FREQUENCY ERROR COMPONENTS IN THE GLOBAL POSITIONING SYSTEM (GPS)/WIDE AREA AUGMENTATION SYSTEM (WAAS) POSITION SOLUTION. [Internet] [Doctoral dissertation]. University of Oklahoma; 2009. [cited 2020 Jan 17]. Available from: http://hdl.handle.net/11244/320318.

Council of Science Editors:

McCartor GR. IDENTIFICATION OF EXTREMELY LOW FREQUENCY ERROR COMPONENTS IN THE GLOBAL POSITIONING SYSTEM (GPS)/WIDE AREA AUGMENTATION SYSTEM (WAAS) POSITION SOLUTION. [Doctoral Dissertation]. University of Oklahoma; 2009. Available from: http://hdl.handle.net/11244/320318


Texas A&M University

8. Oseguera, Rosa Maria. Evaluation of a total energy sensor for glide path control.

Degree: MS, aerospace engineering, 2012, Texas A&M University

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.; Landing aids (Aeronautics) - Testing.; Wind shear.; Detectors - Testing.

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APA (6th Edition):

Oseguera, R. M. (2012). Evaluation of a total energy sensor for glide path control. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1987-THESIS-O81

Chicago Manual of Style (16th Edition):

Oseguera, Rosa Maria. “Evaluation of a total energy sensor for glide path control.” 2012. Masters Thesis, Texas A&M University. Accessed January 17, 2020. http://hdl.handle.net/1969.1/ETD-TAMU-1987-THESIS-O81.

MLA Handbook (7th Edition):

Oseguera, Rosa Maria. “Evaluation of a total energy sensor for glide path control.” 2012. Web. 17 Jan 2020.

Vancouver:

Oseguera RM. Evaluation of a total energy sensor for glide path control. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2020 Jan 17]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1987-THESIS-O81.

Council of Science Editors:

Oseguera RM. Evaluation of a total energy sensor for glide path control. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1987-THESIS-O81


Queensland University of Technology

9. Sang, Jizhang. Theory and development of GPS integrity monitoring system.

Degree: 1996, Queensland University of Technology

 This thesis discusses various aspects of the integrity monitoring of GPS applied to civil aircraft navigation in different phases of flight. These flight phases include… (more)

Subjects/Keywords: Global Positioning System; Landing aids (Aeronautics); Aeronautical instruments; thesis; doctoral

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APA (6th Edition):

Sang, J. (1996). Theory and development of GPS integrity monitoring system. (Thesis). Queensland University of Technology. Retrieved from https://eprints.qut.edu.au/36001/

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):

Sang, Jizhang. “Theory and development of GPS integrity monitoring system.” 1996. Thesis, Queensland University of Technology. Accessed January 17, 2020. https://eprints.qut.edu.au/36001/.

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

MLA Handbook (7th Edition):

Sang, Jizhang. “Theory and development of GPS integrity monitoring system.” 1996. Web. 17 Jan 2020.

Vancouver:

Sang J. Theory and development of GPS integrity monitoring system. [Internet] [Thesis]. Queensland University of Technology; 1996. [cited 2020 Jan 17]. Available from: https://eprints.qut.edu.au/36001/.

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

Council of Science Editors:

Sang J. Theory and development of GPS integrity monitoring system. [Thesis]. Queensland University of Technology; 1996. Available from: https://eprints.qut.edu.au/36001/

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

10. Zhao, Yiming. Efficient and robust aircraft landing trajectory optimization.

Degree: PhD, Aerospace Engineering, 2012, Georgia Tech

 This thesis addresses the challenges in the efficient and robust generation and optimization of three-dimensional landing trajectories for fixed-wing aircraft subject to prescribed boundary conditions… (more)

Subjects/Keywords: Quadratic programming; Optimal control; Trajectory optimization; Aircraft landing; Minimum time; Minimum fuel; Nonlinear programming; Trajectory optimization Mathematical models; Landing aids (Aeronautics); Airplanes Landing

…maneuverability. Therefore, effective automation aids for emergency landing process optimization can… …116 4.6.1 Landing Path with Two Turns . . . . . . . . . . . . . . . . . . . . . 117… …ENERGY-OPTIMAL LANDING PATH TRACKING WITH FIXED TIME OF ARRIVAL… …156 viii VI INITIAL GUESS GENERATION FOR LANDING TRAJECTORY OPTIMIZATION… …158 6.1 Feasible Landing Trajectory Generation . . . . . . . . . . . . . . . . . . . . 158… 

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APA (6th Edition):

Zhao, Y. (2012). Efficient and robust aircraft landing trajectory optimization. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/43586

Chicago Manual of Style (16th Edition):

Zhao, Yiming. “Efficient and robust aircraft landing trajectory optimization.” 2012. Doctoral Dissertation, Georgia Tech. Accessed January 17, 2020. http://hdl.handle.net/1853/43586.

MLA Handbook (7th Edition):

Zhao, Yiming. “Efficient and robust aircraft landing trajectory optimization.” 2012. Web. 17 Jan 2020.

Vancouver:

Zhao Y. Efficient and robust aircraft landing trajectory optimization. [Internet] [Doctoral dissertation]. Georgia Tech; 2012. [cited 2020 Jan 17]. Available from: http://hdl.handle.net/1853/43586.

Council of Science Editors:

Zhao Y. Efficient and robust aircraft landing trajectory optimization. [Doctoral Dissertation]. Georgia Tech; 2012. Available from: http://hdl.handle.net/1853/43586

11. Ward, Michael. Adaptive glide slope control for parafoil and payload aircraft.

Degree: PhD, Aerospace Engineering, 2012, Georgia Tech

 Airdrop systems provide a unique capability of delivering large payloads to undeveloped and inaccessible locations. Traditionally, these systems have been unguided, requiring large landing zones… (more)

Subjects/Keywords: Autonomous; Aircraft; Airdrop; Parafoil; Control; Parachutes; Glide path systems; Landing aids (Aeronautics); Payloads (Aerospace engineering)

…98 Figure 8.3: Predicted Landing Accuracy vs. Wind Speed using only Lateral Control... 100… …Figure 8.4: Predicted Landing Accuracy vs. Wind Speed using Glide Slope Control ... 101 Figure… …8.5: Comparing Predicted Landing Accuracy with Basic Control and with Glide Slope Control… …102 Figure 8.6: Comparing Simulated Landing Accuracy of Basic and Glide Slope Control… …103 Figure 8.7: Landing Dispersions from Autonomous Flight Tests… 

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APA (6th Edition):

Ward, M. (2012). Adaptive glide slope control for parafoil and payload aircraft. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/44710

Chicago Manual of Style (16th Edition):

Ward, Michael. “Adaptive glide slope control for parafoil and payload aircraft.” 2012. Doctoral Dissertation, Georgia Tech. Accessed January 17, 2020. http://hdl.handle.net/1853/44710.

MLA Handbook (7th Edition):

Ward, Michael. “Adaptive glide slope control for parafoil and payload aircraft.” 2012. Web. 17 Jan 2020.

Vancouver:

Ward M. Adaptive glide slope control for parafoil and payload aircraft. [Internet] [Doctoral dissertation]. Georgia Tech; 2012. [cited 2020 Jan 17]. Available from: http://hdl.handle.net/1853/44710.

Council of Science Editors:

Ward M. Adaptive glide slope control for parafoil and payload aircraft. [Doctoral Dissertation]. Georgia Tech; 2012. Available from: http://hdl.handle.net/1853/44710

12. Watts, Robert Michael. Development and evaluation of an automated path planning aid.

Degree: MS, Aerospace Engineering, 2010, Georgia Tech

 In the event of an onboard emergency, air transport pilots are remarkably adept at safely landing their aircraft. However, the tasks of selecting an alternate… (more)

Subjects/Keywords: In-flight emergency; Airplane cockpit design; Cockpit aid; Aerospace human factors; Decision aid; Landing aids (Aeronautics); Trajectory optimization

…Prioritization of Landing Site Criteria for Non-Performance Altering Case… …15 6 Prioritization of Landing Site Criteria for Performance Altering Case. 15 7 Parts… …Distribution of Landing Site Quality. . . . . . . . . . . . . . . . . . . 63 30 Correlation… …safely landing their aircraft. However, the tasks of selecting an alternate landing site and… …dial improved the quality of the selected landing site; however, it also increased the time… 

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APA (6th Edition):

Watts, R. M. (2010). Development and evaluation of an automated path planning aid. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/33839

Chicago Manual of Style (16th Edition):

Watts, Robert Michael. “Development and evaluation of an automated path planning aid.” 2010. Masters Thesis, Georgia Tech. Accessed January 17, 2020. http://hdl.handle.net/1853/33839.

MLA Handbook (7th Edition):

Watts, Robert Michael. “Development and evaluation of an automated path planning aid.” 2010. Web. 17 Jan 2020.

Vancouver:

Watts RM. Development and evaluation of an automated path planning aid. [Internet] [Masters thesis]. Georgia Tech; 2010. [cited 2020 Jan 17]. Available from: http://hdl.handle.net/1853/33839.

Council of Science Editors:

Watts RM. Development and evaluation of an automated path planning aid. [Masters Thesis]. Georgia Tech; 2010. Available from: http://hdl.handle.net/1853/33839


Ohio University

13. Haubeil, J. Jeffrey. Operational viability of a directive distance measuring equipment (DME) antenna in a national airspace system (NAS) approach and landing environment.

Degree: MS, Electrical Engineering & Computer Science (Engineering and Technology), 1996, Ohio University

Operational viability of a directive distance measuring equipment (DME) antenna in a national airspace system (NAS) approach and landing environment Advisors/Committee Members: Braasch, Michael (Advisor).

Subjects/Keywords: Distance Measuring Equipment; National Airspace System; Landing Aids

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APA (6th Edition):

Haubeil, J. J. (1996). Operational viability of a directive distance measuring equipment (DME) antenna in a national airspace system (NAS) approach and landing environment. (Masters Thesis). Ohio University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1178311788

Chicago Manual of Style (16th Edition):

Haubeil, J Jeffrey. “Operational viability of a directive distance measuring equipment (DME) antenna in a national airspace system (NAS) approach and landing environment.” 1996. Masters Thesis, Ohio University. Accessed January 17, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1178311788.

MLA Handbook (7th Edition):

Haubeil, J Jeffrey. “Operational viability of a directive distance measuring equipment (DME) antenna in a national airspace system (NAS) approach and landing environment.” 1996. Web. 17 Jan 2020.

Vancouver:

Haubeil JJ. Operational viability of a directive distance measuring equipment (DME) antenna in a national airspace system (NAS) approach and landing environment. [Internet] [Masters thesis]. Ohio University; 1996. [cited 2020 Jan 17]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1178311788.

Council of Science Editors:

Haubeil JJ. Operational viability of a directive distance measuring equipment (DME) antenna in a national airspace system (NAS) approach and landing environment. [Masters Thesis]. Ohio University; 1996. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1178311788


Virginia Tech

14. Nuhalt, Abdullah O. Numerical simulation of feedback control of aerodynamic configurations in steady and unsteady ground effects.

Degree: PhD, Engineering Mechanics, 1988, Virginia Tech

Subjects/Keywords: LD5655.V856 1988.N842; Runways (Aeronautics)  – Testing; Airplanes  – Landing; Airplanes  – Takeoff

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APA (6th Edition):

Nuhalt, A. O. (1988). Numerical simulation of feedback control of aerodynamic configurations in steady and unsteady ground effects. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/82627

Chicago Manual of Style (16th Edition):

Nuhalt, Abdullah O. “Numerical simulation of feedback control of aerodynamic configurations in steady and unsteady ground effects.” 1988. Doctoral Dissertation, Virginia Tech. Accessed January 17, 2020. http://hdl.handle.net/10919/82627.

MLA Handbook (7th Edition):

Nuhalt, Abdullah O. “Numerical simulation of feedback control of aerodynamic configurations in steady and unsteady ground effects.” 1988. Web. 17 Jan 2020.

Vancouver:

Nuhalt AO. Numerical simulation of feedback control of aerodynamic configurations in steady and unsteady ground effects. [Internet] [Doctoral dissertation]. Virginia Tech; 1988. [cited 2020 Jan 17]. Available from: http://hdl.handle.net/10919/82627.

Council of Science Editors:

Nuhalt AO. Numerical simulation of feedback control of aerodynamic configurations in steady and unsteady ground effects. [Doctoral Dissertation]. Virginia Tech; 1988. Available from: http://hdl.handle.net/10919/82627


MIT

15. Ephrath, Arye Ravoz. Pilot performance in zero-visibility precision approach .

Degree: 1975, MIT

Subjects/Keywords: Aeronautics and Astronautics; Instrument landing systems; Human-machine systems; Air pilots; Airplanes Piloting

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APA (6th Edition):

Ephrath, A. R. (1975). Pilot performance in zero-visibility precision approach . (Thesis). MIT. Retrieved from http://hdl.handle.net/1721.1/27421

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):

Ephrath, Arye Ravoz. “Pilot performance in zero-visibility precision approach .” 1975. Thesis, MIT. Accessed January 17, 2020. http://hdl.handle.net/1721.1/27421.

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

MLA Handbook (7th Edition):

Ephrath, Arye Ravoz. “Pilot performance in zero-visibility precision approach .” 1975. Web. 17 Jan 2020.

Vancouver:

Ephrath AR. Pilot performance in zero-visibility precision approach . [Internet] [Thesis]. MIT; 1975. [cited 2020 Jan 17]. Available from: http://hdl.handle.net/1721.1/27421.

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

Council of Science Editors:

Ephrath AR. Pilot performance in zero-visibility precision approach . [Thesis]. MIT; 1975. Available from: http://hdl.handle.net/1721.1/27421

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


University of Central Florida

16. Lee, Kyongsun. Effects Of Flight Factors On Pilot Performance, Workload, And Stress At Final Approach To Landing Phase Of Flight.

Degree: 2010, University of Central Florida

 Since human errors are one of the major causes of flight accidents, the design and operation of the modern aircraft system deals with them seriously.… (more)

Subjects/Keywords: Aeronautics  – Human factors; Air pilots  – Job stress; Air pilots  – Workload; Airplanes  – Landing  – Simulation methods; Airplanes  – Piloting; Engineering; Dissertations, Academic  – Engineering and Computer Science; Engineering and Computer Science  – Dissertations, Academic

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

APA (6th Edition):

Lee, K. (2010). Effects Of Flight Factors On Pilot Performance, Workload, And Stress At Final Approach To Landing Phase Of Flight. (Doctoral Dissertation). University of Central Florida. Retrieved from https://stars.library.ucf.edu/etd/1628

Chicago Manual of Style (16th Edition):

Lee, Kyongsun. “Effects Of Flight Factors On Pilot Performance, Workload, And Stress At Final Approach To Landing Phase Of Flight.” 2010. Doctoral Dissertation, University of Central Florida. Accessed January 17, 2020. https://stars.library.ucf.edu/etd/1628.

MLA Handbook (7th Edition):

Lee, Kyongsun. “Effects Of Flight Factors On Pilot Performance, Workload, And Stress At Final Approach To Landing Phase Of Flight.” 2010. Web. 17 Jan 2020.

Vancouver:

Lee K. Effects Of Flight Factors On Pilot Performance, Workload, And Stress At Final Approach To Landing Phase Of Flight. [Internet] [Doctoral dissertation]. University of Central Florida; 2010. [cited 2020 Jan 17]. Available from: https://stars.library.ucf.edu/etd/1628.

Council of Science Editors:

Lee K. Effects Of Flight Factors On Pilot Performance, Workload, And Stress At Final Approach To Landing Phase Of Flight. [Doctoral Dissertation]. University of Central Florida; 2010. Available from: https://stars.library.ucf.edu/etd/1628


Virginia Tech

17. Nam, Amadou Sylla. Increasing capacity by the use of optimal runway exits, automated landing, roll out and turnoff in an airport environment.

Degree: MS, Civil Engineering, 1986, Virginia Tech

Subjects/Keywords: LD5655.V855 1986.N352; Airports  – Traffic control  – Data processing; Runways (Aeronautics); Airplanes  – Landing

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APA (6th Edition):

Nam, A. S. (1986). Increasing capacity by the use of optimal runway exits, automated landing, roll out and turnoff in an airport environment. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/90951

Chicago Manual of Style (16th Edition):

Nam, Amadou Sylla. “Increasing capacity by the use of optimal runway exits, automated landing, roll out and turnoff in an airport environment.” 1986. Masters Thesis, Virginia Tech. Accessed January 17, 2020. http://hdl.handle.net/10919/90951.

MLA Handbook (7th Edition):

Nam, Amadou Sylla. “Increasing capacity by the use of optimal runway exits, automated landing, roll out and turnoff in an airport environment.” 1986. Web. 17 Jan 2020.

Vancouver:

Nam AS. Increasing capacity by the use of optimal runway exits, automated landing, roll out and turnoff in an airport environment. [Internet] [Masters thesis]. Virginia Tech; 1986. [cited 2020 Jan 17]. Available from: http://hdl.handle.net/10919/90951.

Council of Science Editors:

Nam AS. Increasing capacity by the use of optimal runway exits, automated landing, roll out and turnoff in an airport environment. [Masters Thesis]. Virginia Tech; 1986. Available from: http://hdl.handle.net/10919/90951


Virginia Tech

18. Eppard, William M. Integrated aerodynamic-structural design optimization.

Degree: MS, Aerospace Engineering, 1987, Virginia Tech

Subjects/Keywords: LD5655.V855 1987.E67; Aerodynamics; Gliders (Aeronautics)  – Design; Landing craft  – Design and construction

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APA (6th Edition):

Eppard, W. M. (1987). Integrated aerodynamic-structural design optimization. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/90966

Chicago Manual of Style (16th Edition):

Eppard, William M. “Integrated aerodynamic-structural design optimization.” 1987. Masters Thesis, Virginia Tech. Accessed January 17, 2020. http://hdl.handle.net/10919/90966.

MLA Handbook (7th Edition):

Eppard, William M. “Integrated aerodynamic-structural design optimization.” 1987. Web. 17 Jan 2020.

Vancouver:

Eppard WM. Integrated aerodynamic-structural design optimization. [Internet] [Masters thesis]. Virginia Tech; 1987. [cited 2020 Jan 17]. Available from: http://hdl.handle.net/10919/90966.

Council of Science Editors:

Eppard WM. Integrated aerodynamic-structural design optimization. [Masters Thesis]. Virginia Tech; 1987. Available from: http://hdl.handle.net/10919/90966


Virginia Tech

19. Kim, Byung Jong. Optimal runway exit design and capacity enhancement.

Degree: PhD, Civil Engineering, 1993, Virginia Tech

 Congestion and delay problems at airports have received much attention in recent years because of the unbalanced condition between demand and supply. Recent demand forecasts… (more)

Subjects/Keywords: Airplanes Landing Mathematical models; Runways (Aeronautics) Design; LD5655.V856 1993.K56

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APA (6th Edition):

Kim, B. J. (1993). Optimal runway exit design and capacity enhancement. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/38637

Chicago Manual of Style (16th Edition):

Kim, Byung Jong. “Optimal runway exit design and capacity enhancement.” 1993. Doctoral Dissertation, Virginia Tech. Accessed January 17, 2020. http://hdl.handle.net/10919/38637.

MLA Handbook (7th Edition):

Kim, Byung Jong. “Optimal runway exit design and capacity enhancement.” 1993. Web. 17 Jan 2020.

Vancouver:

Kim BJ. Optimal runway exit design and capacity enhancement. [Internet] [Doctoral dissertation]. Virginia Tech; 1993. [cited 2020 Jan 17]. Available from: http://hdl.handle.net/10919/38637.

Council of Science Editors:

Kim BJ. Optimal runway exit design and capacity enhancement. [Doctoral Dissertation]. Virginia Tech; 1993. Available from: http://hdl.handle.net/10919/38637


Univerzitet u Beogradu

20. Marčeta, Dušan M. Mogućnosti i optimizacija sletanja na južnu hemisferu Marsa.

Degree: Matematički fakultet, 2016, Univerzitet u Beogradu

Astronomija / Astronomy

Skoro 40 godina nakon prvog uspesnog sletanja na Mars, istrazivanje njegove povrsine pomocu kosmickih letelica i dalje predstavlja ogroman naucni i tehnoloski… (more)

Subjects/Keywords: Mars; atmosphere; landing

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APA (6th Edition):

Marčeta, D. M. (2016). Mogućnosti i optimizacija sletanja na južnu hemisferu Marsa. (Thesis). Univerzitet u Beogradu. Retrieved from https://fedorabg.bg.ac.rs/fedora/get/o:11265/bdef:Content/get

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):

Marčeta, Dušan M. “Mogućnosti i optimizacija sletanja na južnu hemisferu Marsa.” 2016. Thesis, Univerzitet u Beogradu. Accessed January 17, 2020. https://fedorabg.bg.ac.rs/fedora/get/o:11265/bdef:Content/get.

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

MLA Handbook (7th Edition):

Marčeta, Dušan M. “Mogućnosti i optimizacija sletanja na južnu hemisferu Marsa.” 2016. Web. 17 Jan 2020.

Vancouver:

Marčeta DM. Mogućnosti i optimizacija sletanja na južnu hemisferu Marsa. [Internet] [Thesis]. Univerzitet u Beogradu; 2016. [cited 2020 Jan 17]. Available from: https://fedorabg.bg.ac.rs/fedora/get/o:11265/bdef:Content/get.

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

Council of Science Editors:

Marčeta DM. Mogućnosti i optimizacija sletanja na južnu hemisferu Marsa. [Thesis]. Univerzitet u Beogradu; 2016. Available from: https://fedorabg.bg.ac.rs/fedora/get/o:11265/bdef:Content/get

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


University of New South Wales

21. Hayes, Peter. Stability Requirements of Naval Landing Craft.

Degree: Engineering & Information Technology, 2014, University of New South Wales

Landing craft have been operated by various navies around the world, including the Royal Australian Navy (RAN), for many decades to transport vehicles and personnel,… (more)

Subjects/Keywords: Landing Craft; Stability

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APA (6th Edition):

Hayes, P. (2014). Stability Requirements of Naval Landing Craft. (Masters Thesis). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/53853 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:12558/SOURCE02?view=true

Chicago Manual of Style (16th Edition):

Hayes, Peter. “Stability Requirements of Naval Landing Craft.” 2014. Masters Thesis, University of New South Wales. Accessed January 17, 2020. http://handle.unsw.edu.au/1959.4/53853 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:12558/SOURCE02?view=true.

MLA Handbook (7th Edition):

Hayes, Peter. “Stability Requirements of Naval Landing Craft.” 2014. Web. 17 Jan 2020.

Vancouver:

Hayes P. Stability Requirements of Naval Landing Craft. [Internet] [Masters thesis]. University of New South Wales; 2014. [cited 2020 Jan 17]. Available from: http://handle.unsw.edu.au/1959.4/53853 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:12558/SOURCE02?view=true.

Council of Science Editors:

Hayes P. Stability Requirements of Naval Landing Craft. [Masters Thesis]. University of New South Wales; 2014. Available from: http://handle.unsw.edu.au/1959.4/53853 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:12558/SOURCE02?view=true

22. Acree, Cecil Wallace. Pilot estimates of glide path and aim point during simulated landing approaches .

Degree: 1978, MIT

Subjects/Keywords: Aeronautics and Astronautics; Airplanes Landing; Airplanes Piloting; Flight simulators; Glide path systems

…Construction of a model of a pilot's visual information processing during VFR landing… …accidents occur during the 2% of flight time spent in approach and landing (Hasbrook, 1975… …was to obtain the perceptual responses of humans to deviations from a nominal landing… …perceptions, so only brief segments of landing approaches were actually shown to the subjects, and… …scenes onto the screen, simulating the view out of a real aircraft during a landing approach… 

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

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APA (6th Edition):

Acree, C. W. (1978). Pilot estimates of glide path and aim point during simulated landing approaches . (Thesis). MIT. Retrieved from http://hdl.handle.net/1721.1/83649

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):

Acree, Cecil Wallace. “Pilot estimates of glide path and aim point during simulated landing approaches .” 1978. Thesis, MIT. Accessed January 17, 2020. http://hdl.handle.net/1721.1/83649.

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

MLA Handbook (7th Edition):

Acree, Cecil Wallace. “Pilot estimates of glide path and aim point during simulated landing approaches .” 1978. Web. 17 Jan 2020.

Vancouver:

Acree CW. Pilot estimates of glide path and aim point during simulated landing approaches . [Internet] [Thesis]. MIT; 1978. [cited 2020 Jan 17]. Available from: http://hdl.handle.net/1721.1/83649.

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

Council of Science Editors:

Acree CW. Pilot estimates of glide path and aim point during simulated landing approaches . [Thesis]. MIT; 1978. Available from: http://hdl.handle.net/1721.1/83649

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


MIT

23. Stephens, Albert Thomas. Instrument scan, performance, and mental workload in aircraft pilots .

Degree: MS, Aeronautics and Astronautics, 1981, MIT

Subjects/Keywords: Aeronautics and Astronautics.; Air pilots; Flight Physiological aspects; Aviation psychology; Flight simulators; Instrument landing systems

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APA (6th Edition):

Stephens, A. T. (1981). Instrument scan, performance, and mental workload in aircraft pilots . (Masters Thesis). MIT. Retrieved from http://hdl.handle.net/1721.1/15855

Chicago Manual of Style (16th Edition):

Stephens, Albert Thomas. “Instrument scan, performance, and mental workload in aircraft pilots .” 1981. Masters Thesis, MIT. Accessed January 17, 2020. http://hdl.handle.net/1721.1/15855.

MLA Handbook (7th Edition):

Stephens, Albert Thomas. “Instrument scan, performance, and mental workload in aircraft pilots .” 1981. Web. 17 Jan 2020.

Vancouver:

Stephens AT. Instrument scan, performance, and mental workload in aircraft pilots . [Internet] [Masters thesis]. MIT; 1981. [cited 2020 Jan 17]. Available from: http://hdl.handle.net/1721.1/15855.

Council of Science Editors:

Stephens AT. Instrument scan, performance, and mental workload in aircraft pilots . [Masters Thesis]. MIT; 1981. Available from: http://hdl.handle.net/1721.1/15855


University of Utah

24. Linn, Braden Kyle. Interdependence of systems of dominance, place theory and gender in creating risk factors for HIV.

Degree: Master of City and Metropolitan Planning;, Architecture & Planning (College of);, 2009, University of Utah

 Existing research in HIV prevention typically focuses on increasing personal agency to overcome risk factors. My research focuses on structural risk factors and policy changes… (more)

Subjects/Keywords: AIDS

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APA (6th Edition):

Linn, B. K. (2009). Interdependence of systems of dominance, place theory and gender in creating risk factors for HIV. (Masters Thesis). University of Utah. Retrieved from http://content.lib.utah.edu/cdm/singleitem/collection/etd2/id/85/rec/656

Chicago Manual of Style (16th Edition):

Linn, Braden Kyle. “Interdependence of systems of dominance, place theory and gender in creating risk factors for HIV.” 2009. Masters Thesis, University of Utah. Accessed January 17, 2020. http://content.lib.utah.edu/cdm/singleitem/collection/etd2/id/85/rec/656.

MLA Handbook (7th Edition):

Linn, Braden Kyle. “Interdependence of systems of dominance, place theory and gender in creating risk factors for HIV.” 2009. Web. 17 Jan 2020.

Vancouver:

Linn BK. Interdependence of systems of dominance, place theory and gender in creating risk factors for HIV. [Internet] [Masters thesis]. University of Utah; 2009. [cited 2020 Jan 17]. Available from: http://content.lib.utah.edu/cdm/singleitem/collection/etd2/id/85/rec/656.

Council of Science Editors:

Linn BK. Interdependence of systems of dominance, place theory and gender in creating risk factors for HIV. [Masters Thesis]. University of Utah; 2009. Available from: http://content.lib.utah.edu/cdm/singleitem/collection/etd2/id/85/rec/656


University of Alberta

25. Moolyk, Amy Nicole. Energetics of weightlifting and jump landing tasks.

Degree: MS, Physical Education and Recreation, 2012, University of Alberta

 The objective of this research was to study the work performed and distribution of work across the lower extremity in various landing tasks. Ten women… (more)

Subjects/Keywords: landing; energetics; weightlifting; biomechanics

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APA (6th Edition):

Moolyk, A. N. (2012). Energetics of weightlifting and jump landing tasks. (Masters Thesis). University of Alberta. Retrieved from https://era.library.ualberta.ca/files/9c67wn622

Chicago Manual of Style (16th Edition):

Moolyk, Amy Nicole. “Energetics of weightlifting and jump landing tasks.” 2012. Masters Thesis, University of Alberta. Accessed January 17, 2020. https://era.library.ualberta.ca/files/9c67wn622.

MLA Handbook (7th Edition):

Moolyk, Amy Nicole. “Energetics of weightlifting and jump landing tasks.” 2012. Web. 17 Jan 2020.

Vancouver:

Moolyk AN. Energetics of weightlifting and jump landing tasks. [Internet] [Masters thesis]. University of Alberta; 2012. [cited 2020 Jan 17]. Available from: https://era.library.ualberta.ca/files/9c67wn622.

Council of Science Editors:

Moolyk AN. Energetics of weightlifting and jump landing tasks. [Masters Thesis]. University of Alberta; 2012. Available from: https://era.library.ualberta.ca/files/9c67wn622


Texas A&M University

26. 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 January 17, 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. 17 Jan 2020.

Vancouver:

Ding Y. Decentralized aircraft landing scheduling at single runway non-controlled airports. [Internet] [Thesis]. Texas A&M University; 2009. [cited 2020 Jan 17]. 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


Brigham Young University

27. Wynn, Jesse Stewart. Visual Servoing for Precision Shipboard Landing of an Autonomous Multirotor Aircraft System.

Degree: MS, 2018, Brigham Young University

 Precision landing capability is a necessary development that must take place before unmanned aircraft systems (UAS) can realize their full potential in today's modern society.… (more)

Subjects/Keywords: visual servoing; quadrotor control; autonomous landing; precision landing; shipboard landing; maritime landing; computer vision; feed-forward; multirotor; autonomy; Kalman filter; Engineering

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APA (6th Edition):

Wynn, J. S. (2018). Visual Servoing for Precision Shipboard Landing of an Autonomous Multirotor Aircraft System. (Masters Thesis). Brigham Young University. Retrieved from https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=8112&context=etd

Chicago Manual of Style (16th Edition):

Wynn, Jesse Stewart. “Visual Servoing for Precision Shipboard Landing of an Autonomous Multirotor Aircraft System.” 2018. Masters Thesis, Brigham Young University. Accessed January 17, 2020. https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=8112&context=etd.

MLA Handbook (7th Edition):

Wynn, Jesse Stewart. “Visual Servoing for Precision Shipboard Landing of an Autonomous Multirotor Aircraft System.” 2018. Web. 17 Jan 2020.

Vancouver:

Wynn JS. Visual Servoing for Precision Shipboard Landing of an Autonomous Multirotor Aircraft System. [Internet] [Masters thesis]. Brigham Young University; 2018. [cited 2020 Jan 17]. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=8112&context=etd.

Council of Science Editors:

Wynn JS. Visual Servoing for Precision Shipboard Landing of an Autonomous Multirotor Aircraft System. [Masters Thesis]. Brigham Young University; 2018. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=8112&context=etd


Virginia Tech

28. Roback, Vincent Eric. Characterization and Helicopter Flight Test of 3-D Imaging Flash LIDAR Technology for Safe, Autonomous, and Precise Planetary Landing.

Degree: MS, Electrical and Computer Engineering, 2012, Virginia Tech

 Two flash lidars, integrated from a number of cutting-edge components from industry and NASA, are lab characterized and flight tested under the Autonomous Landing and… (more)

Subjects/Keywords: Precision Landing; Safe Landing; 3-D Imaging; Flash Lidar; Laser Remote Sensing; Hazard Detection; ALHAT; Flight Test; Planetary Landing; Lunar Landing

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APA (6th Edition):

Roback, V. E. (2012). Characterization and Helicopter Flight Test of 3-D Imaging Flash LIDAR Technology for Safe, Autonomous, and Precise Planetary Landing. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/76845

Chicago Manual of Style (16th Edition):

Roback, Vincent Eric. “Characterization and Helicopter Flight Test of 3-D Imaging Flash LIDAR Technology for Safe, Autonomous, and Precise Planetary Landing.” 2012. Masters Thesis, Virginia Tech. Accessed January 17, 2020. http://hdl.handle.net/10919/76845.

MLA Handbook (7th Edition):

Roback, Vincent Eric. “Characterization and Helicopter Flight Test of 3-D Imaging Flash LIDAR Technology for Safe, Autonomous, and Precise Planetary Landing.” 2012. Web. 17 Jan 2020.

Vancouver:

Roback VE. Characterization and Helicopter Flight Test of 3-D Imaging Flash LIDAR Technology for Safe, Autonomous, and Precise Planetary Landing. [Internet] [Masters thesis]. Virginia Tech; 2012. [cited 2020 Jan 17]. Available from: http://hdl.handle.net/10919/76845.

Council of Science Editors:

Roback VE. Characterization and Helicopter Flight Test of 3-D Imaging Flash LIDAR Technology for Safe, Autonomous, and Precise Planetary Landing. [Masters Thesis]. Virginia Tech; 2012. Available from: http://hdl.handle.net/10919/76845

29. 田村, 嘉章. 画像を用いた月惑星表面への着陸航法.

Degree: 2017, The University of Tokyo / 東京大学

 For an unmanned exploration on the moon or a planet, an autonomous lander is necessary. This paper describes a method to recognize obstacles on the… (more)

Subjects/Keywords: landing; image

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APA (6th Edition):

田村, . (2017). 画像を用いた月惑星表面への着陸航法. (Thesis). The University of Tokyo / 東京大学. Retrieved from http://hdl.handle.net/2261/26295

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):

田村, 嘉章. “画像を用いた月惑星表面への着陸航法.” 2017. Thesis, The University of Tokyo / 東京大学. Accessed January 17, 2020. http://hdl.handle.net/2261/26295.

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

MLA Handbook (7th Edition):

田村, 嘉章. “画像を用いた月惑星表面への着陸航法.” 2017. Web. 17 Jan 2020.

Vancouver:

田村 . 画像を用いた月惑星表面への着陸航法. [Internet] [Thesis]. The University of Tokyo / 東京大学; 2017. [cited 2020 Jan 17]. Available from: http://hdl.handle.net/2261/26295.

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

Council of Science Editors:

田村 . 画像を用いた月惑星表面への着陸航法. [Thesis]. The University of Tokyo / 東京大学; 2017. Available from: http://hdl.handle.net/2261/26295

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


University of North Texas

30. Aguilar Ayala, Roberto. Applications of Metallic Clusters and Nanoparticles via Soft Landing Ion Mobility, from Reduced to Ambient Pressures.

Degree: 2018, University of North Texas

 Nanoparticles, simple yet groundbreaking objects have led to the discovery of invaluable information due to their physiological, chemical, and physical properties, have become a hot… (more)

Subjects/Keywords: soft-landing; nanoparticles; mass spectrometry

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APA (6th Edition):

Aguilar Ayala, R. (2018). Applications of Metallic Clusters and Nanoparticles via Soft Landing Ion Mobility, from Reduced to Ambient Pressures. (Thesis). University of North Texas. Retrieved from https://digital.library.unt.edu/ark:/67531/metadc1248434/

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):

Aguilar Ayala, Roberto. “Applications of Metallic Clusters and Nanoparticles via Soft Landing Ion Mobility, from Reduced to Ambient Pressures.” 2018. Thesis, University of North Texas. Accessed January 17, 2020. https://digital.library.unt.edu/ark:/67531/metadc1248434/.

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

MLA Handbook (7th Edition):

Aguilar Ayala, Roberto. “Applications of Metallic Clusters and Nanoparticles via Soft Landing Ion Mobility, from Reduced to Ambient Pressures.” 2018. Web. 17 Jan 2020.

Vancouver:

Aguilar Ayala R. Applications of Metallic Clusters and Nanoparticles via Soft Landing Ion Mobility, from Reduced to Ambient Pressures. [Internet] [Thesis]. University of North Texas; 2018. [cited 2020 Jan 17]. Available from: https://digital.library.unt.edu/ark:/67531/metadc1248434/.

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

Council of Science Editors:

Aguilar Ayala R. Applications of Metallic Clusters and Nanoparticles via Soft Landing Ion Mobility, from Reduced to Ambient Pressures. [Thesis]. University of North Texas; 2018. Available from: https://digital.library.unt.edu/ark:/67531/metadc1248434/

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

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