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You searched for subject:( Trajectory Optimization). Showing records 1 – 30 of 198 total matches.

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Delft University of Technology

1. Zhong, Z. Optimal long-haul Trajectories in a Wind Field:.

Degree: 2014, Delft University of Technology

 The long-haul flights of airlines are impacted by the en-route wind fields. Flights on the same route with different directions may have significantly different flight… (more)

Subjects/Keywords: trajectory optimization

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

APA (6th Edition):

Zhong, Z. (2014). Optimal long-haul Trajectories in a Wind Field:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:35dd7fd7-6e66-45c5-97b6-4be811cbcf65

Chicago Manual of Style (16th Edition):

Zhong, Z. “Optimal long-haul Trajectories in a Wind Field:.” 2014. Masters Thesis, Delft University of Technology. Accessed March 25, 2019. http://resolver.tudelft.nl/uuid:35dd7fd7-6e66-45c5-97b6-4be811cbcf65.

MLA Handbook (7th Edition):

Zhong, Z. “Optimal long-haul Trajectories in a Wind Field:.” 2014. Web. 25 Mar 2019.

Vancouver:

Zhong Z. Optimal long-haul Trajectories in a Wind Field:. [Internet] [Masters thesis]. Delft University of Technology; 2014. [cited 2019 Mar 25]. Available from: http://resolver.tudelft.nl/uuid:35dd7fd7-6e66-45c5-97b6-4be811cbcf65.

Council of Science Editors:

Zhong Z. Optimal long-haul Trajectories in a Wind Field:. [Masters Thesis]. Delft University of Technology; 2014. Available from: http://resolver.tudelft.nl/uuid:35dd7fd7-6e66-45c5-97b6-4be811cbcf65


University of Waterloo

2. Chen, Christina (Qing Ge). Time-Optimal Feedrate Planning for Freeform Toolpaths for Manufacturing Applications.

Degree: 2018, University of Waterloo

 Optimality and computational efficiency are two desired yet competing attributes of time-optimal feedrate planning. A well-designed algorithm can vastly increase machining productivity, by reducing tool… (more)

Subjects/Keywords: Trajectory Optimization; CNC

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APA (6th Edition):

Chen, C. (. G. (2018). Time-Optimal Feedrate Planning for Freeform Toolpaths for Manufacturing Applications. (Thesis). University of Waterloo. Retrieved from http://hdl.handle.net/10012/13040

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):

Chen, Christina (Qing Ge). “Time-Optimal Feedrate Planning for Freeform Toolpaths for Manufacturing Applications.” 2018. Thesis, University of Waterloo. Accessed March 25, 2019. http://hdl.handle.net/10012/13040.

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

MLA Handbook (7th Edition):

Chen, Christina (Qing Ge). “Time-Optimal Feedrate Planning for Freeform Toolpaths for Manufacturing Applications.” 2018. Web. 25 Mar 2019.

Vancouver:

Chen C(G. Time-Optimal Feedrate Planning for Freeform Toolpaths for Manufacturing Applications. [Internet] [Thesis]. University of Waterloo; 2018. [cited 2019 Mar 25]. Available from: http://hdl.handle.net/10012/13040.

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

Council of Science Editors:

Chen C(G. Time-Optimal Feedrate Planning for Freeform Toolpaths for Manufacturing Applications. [Thesis]. University of Waterloo; 2018. Available from: http://hdl.handle.net/10012/13040

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


Texas A&M University

3. Kim, Sung Hyun. Multi-layer approach to motion planning in obstacle rich environment.

Degree: 2009, Texas A&M University

 A widespread use of robotic technology in civilian and military applications has generated a need for advanced motion planning algorithms that are real-time implementable. These… (more)

Subjects/Keywords: motion planning; trajectory optimization; robotics

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APA (6th Edition):

Kim, S. H. (2009). Multi-layer approach to motion planning in obstacle rich environment. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2621

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):

Kim, Sung Hyun. “Multi-layer approach to motion planning in obstacle rich environment.” 2009. Thesis, Texas A&M University. Accessed March 25, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2621.

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

MLA Handbook (7th Edition):

Kim, Sung Hyun. “Multi-layer approach to motion planning in obstacle rich environment.” 2009. Web. 25 Mar 2019.

Vancouver:

Kim SH. Multi-layer approach to motion planning in obstacle rich environment. [Internet] [Thesis]. Texas A&M University; 2009. [cited 2019 Mar 25]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2621.

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

Council of Science Editors:

Kim SH. Multi-layer approach to motion planning in obstacle rich environment. [Thesis]. Texas A&M University; 2009. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2621

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


Cornell University

4. Kogan, Boris. Controlled Ballistic Trajectory For Small Caliber Spin-Stabilized Smart Munitions .

Degree: 2014, Cornell University

 The dynamics of bullets is examined to develop an approach for their active controls. The precession and nutation is observed to be the dominant modes… (more)

Subjects/Keywords: ballistics; bullets; trajectory optimization

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APA (6th Edition):

Kogan, B. (2014). Controlled Ballistic Trajectory For Small Caliber Spin-Stabilized Smart Munitions . (Thesis). Cornell University. Retrieved from http://hdl.handle.net/1813/37027

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):

Kogan, Boris. “Controlled Ballistic Trajectory For Small Caliber Spin-Stabilized Smart Munitions .” 2014. Thesis, Cornell University. Accessed March 25, 2019. http://hdl.handle.net/1813/37027.

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

MLA Handbook (7th Edition):

Kogan, Boris. “Controlled Ballistic Trajectory For Small Caliber Spin-Stabilized Smart Munitions .” 2014. Web. 25 Mar 2019.

Vancouver:

Kogan B. Controlled Ballistic Trajectory For Small Caliber Spin-Stabilized Smart Munitions . [Internet] [Thesis]. Cornell University; 2014. [cited 2019 Mar 25]. Available from: http://hdl.handle.net/1813/37027.

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

Council of Science Editors:

Kogan B. Controlled Ballistic Trajectory For Small Caliber Spin-Stabilized Smart Munitions . [Thesis]. Cornell University; 2014. Available from: http://hdl.handle.net/1813/37027

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


Delft University of Technology

5. Oldenhuis, R.P.S. Trajectory Optimization for a Mission to the Solar Bow Shock and Minor Planets:.

Degree: 2010, Delft University of Technology

 In November 2003 the Voyager 1 spacecraft pierced through the Solar system’s termination shock, followed by Voyager 2 in August 2007. These events marked the… (more)

Subjects/Keywords: Trajectory optimization; Minor Planet; Interstellar

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APA (6th Edition):

Oldenhuis, R. P. S. (2010). Trajectory Optimization for a Mission to the Solar Bow Shock and Minor Planets:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:6672aa53-6ecc-4571-85b2-2d4aafbba5bd

Chicago Manual of Style (16th Edition):

Oldenhuis, R P S. “Trajectory Optimization for a Mission to the Solar Bow Shock and Minor Planets:.” 2010. Masters Thesis, Delft University of Technology. Accessed March 25, 2019. http://resolver.tudelft.nl/uuid:6672aa53-6ecc-4571-85b2-2d4aafbba5bd.

MLA Handbook (7th Edition):

Oldenhuis, R P S. “Trajectory Optimization for a Mission to the Solar Bow Shock and Minor Planets:.” 2010. Web. 25 Mar 2019.

Vancouver:

Oldenhuis RPS. Trajectory Optimization for a Mission to the Solar Bow Shock and Minor Planets:. [Internet] [Masters thesis]. Delft University of Technology; 2010. [cited 2019 Mar 25]. Available from: http://resolver.tudelft.nl/uuid:6672aa53-6ecc-4571-85b2-2d4aafbba5bd.

Council of Science Editors:

Oldenhuis RPS. Trajectory Optimization for a Mission to the Solar Bow Shock and Minor Planets:. [Masters Thesis]. Delft University of Technology; 2010. Available from: http://resolver.tudelft.nl/uuid:6672aa53-6ecc-4571-85b2-2d4aafbba5bd


Mississippi State University

6. Zhou, Fang. A parsimonious two-way shooting algorithm for connected automated traffic smoothing.

Degree: MS, Civil and Environmental Engineering, 2015, Mississippi State University

  Advanced connected and automated vehicle technologies offer new opportunities for highway traffic smoothing by optimizing automated vehicle trajectories. As one of the pioneering attempts,… (more)

Subjects/Keywords: Connected; Automated; trajectory optimization; heuristic

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APA (6th Edition):

Zhou, F. (2015). A parsimonious two-way shooting algorithm for connected automated traffic smoothing. (Masters Thesis). Mississippi State University. Retrieved from http://sun.library.msstate.edu/ETD-db/theses/available/etd-04232015-145513/ ;

Chicago Manual of Style (16th Edition):

Zhou, Fang. “A parsimonious two-way shooting algorithm for connected automated traffic smoothing.” 2015. Masters Thesis, Mississippi State University. Accessed March 25, 2019. http://sun.library.msstate.edu/ETD-db/theses/available/etd-04232015-145513/ ;.

MLA Handbook (7th Edition):

Zhou, Fang. “A parsimonious two-way shooting algorithm for connected automated traffic smoothing.” 2015. Web. 25 Mar 2019.

Vancouver:

Zhou F. A parsimonious two-way shooting algorithm for connected automated traffic smoothing. [Internet] [Masters thesis]. Mississippi State University; 2015. [cited 2019 Mar 25]. Available from: http://sun.library.msstate.edu/ETD-db/theses/available/etd-04232015-145513/ ;.

Council of Science Editors:

Zhou F. A parsimonious two-way shooting algorithm for connected automated traffic smoothing. [Masters Thesis]. Mississippi State University; 2015. Available from: http://sun.library.msstate.edu/ETD-db/theses/available/etd-04232015-145513/ ;


University of Missouri – Columbia

7. Huang, Weijun. Optimal orbit transfers for satellite formation flying applications.

Degree: 2012, University of Missouri – Columbia

 This dissertation focused on trajectory optimization problems arising from the application of satellite formation flying, and obtained three major results. First, the dissertation proposed an… (more)

Subjects/Keywords: trajectory optimization; fuel-optimal trajectory; impulsive trajectory; linearization method

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APA (6th Edition):

Huang, W. (2012). Optimal orbit transfers for satellite formation flying applications. (Thesis). University of Missouri – Columbia. Retrieved from http://hdl.handle.net/10355/36670

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):

Huang, Weijun. “Optimal orbit transfers for satellite formation flying applications.” 2012. Thesis, University of Missouri – Columbia. Accessed March 25, 2019. http://hdl.handle.net/10355/36670.

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

MLA Handbook (7th Edition):

Huang, Weijun. “Optimal orbit transfers for satellite formation flying applications.” 2012. Web. 25 Mar 2019.

Vancouver:

Huang W. Optimal orbit transfers for satellite formation flying applications. [Internet] [Thesis]. University of Missouri – Columbia; 2012. [cited 2019 Mar 25]. Available from: http://hdl.handle.net/10355/36670.

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

Council of Science Editors:

Huang W. Optimal orbit transfers for satellite formation flying applications. [Thesis]. University of Missouri – Columbia; 2012. Available from: http://hdl.handle.net/10355/36670

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


Hong Kong University of Science and Technology

8. Zhang, Wei. Calibration of GPS trajectory datasets.

Degree: 2010, Hong Kong University of Science and Technology

 An accurate and high-sampling-rate GPS trajectory dataset is essential to many trajectory-based applications. However, in practice the GPS dataset always has large position errors and… (more)

Subjects/Keywords: Global Positioning System  – Data processing; Trajectory optimization

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APA (6th Edition):

Zhang, W. (2010). Calibration of GPS trajectory datasets. (Thesis). Hong Kong University of Science and Technology. Retrieved from https://doi.org/10.14711/thesis-b1114955 ; http://repository.ust.hk/ir/bitstream/1783.1-6944/1/th_redirect.html

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):

Zhang, Wei. “Calibration of GPS trajectory datasets.” 2010. Thesis, Hong Kong University of Science and Technology. Accessed March 25, 2019. https://doi.org/10.14711/thesis-b1114955 ; http://repository.ust.hk/ir/bitstream/1783.1-6944/1/th_redirect.html.

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

MLA Handbook (7th Edition):

Zhang, Wei. “Calibration of GPS trajectory datasets.” 2010. Web. 25 Mar 2019.

Vancouver:

Zhang W. Calibration of GPS trajectory datasets. [Internet] [Thesis]. Hong Kong University of Science and Technology; 2010. [cited 2019 Mar 25]. Available from: https://doi.org/10.14711/thesis-b1114955 ; http://repository.ust.hk/ir/bitstream/1783.1-6944/1/th_redirect.html.

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

Council of Science Editors:

Zhang W. Calibration of GPS trajectory datasets. [Thesis]. Hong Kong University of Science and Technology; 2010. Available from: https://doi.org/10.14711/thesis-b1114955 ; http://repository.ust.hk/ir/bitstream/1783.1-6944/1/th_redirect.html

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


Penn State University

9. Tu, Chenmeng. Application of a Homotopy Method to Low-Thrust Trajectory Optimization.

Degree: MS, Aerospace Engineering, 2008, Penn State University

 Continuous optimization methods, historically classified into direct and indirect method categories, have demonstrated notable success in continuous-thrust trajectory optimization. An optimization problem is transformed into… (more)

Subjects/Keywords: Trajectory Optimization; Low-Thrust; Homotopy Method

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APA (6th Edition):

Tu, C. (2008). Application of a Homotopy Method to Low-Thrust Trajectory Optimization. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/8862

Chicago Manual of Style (16th Edition):

Tu, Chenmeng. “Application of a Homotopy Method to Low-Thrust Trajectory Optimization.” 2008. Masters Thesis, Penn State University. Accessed March 25, 2019. https://etda.libraries.psu.edu/catalog/8862.

MLA Handbook (7th Edition):

Tu, Chenmeng. “Application of a Homotopy Method to Low-Thrust Trajectory Optimization.” 2008. Web. 25 Mar 2019.

Vancouver:

Tu C. Application of a Homotopy Method to Low-Thrust Trajectory Optimization. [Internet] [Masters thesis]. Penn State University; 2008. [cited 2019 Mar 25]. Available from: https://etda.libraries.psu.edu/catalog/8862.

Council of Science Editors:

Tu C. Application of a Homotopy Method to Low-Thrust Trajectory Optimization. [Masters Thesis]. Penn State University; 2008. Available from: https://etda.libraries.psu.edu/catalog/8862


Cornell University

10. Kelly, Matthew. Designing Reliable Controllers For Bipedal Robots .

Degree: 2016, Cornell University

 This dissertation is made up of several chapters, each of which is a stand-alone document. Together, these chapters are representative of my research here at… (more)

Subjects/Keywords: Nonlinear Control; Trajectory Optimization; Walking Robots

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APA (6th Edition):

Kelly, M. (2016). Designing Reliable Controllers For Bipedal Robots . (Thesis). Cornell University. Retrieved from http://hdl.handle.net/1813/44350

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):

Kelly, Matthew. “Designing Reliable Controllers For Bipedal Robots .” 2016. Thesis, Cornell University. Accessed March 25, 2019. http://hdl.handle.net/1813/44350.

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

MLA Handbook (7th Edition):

Kelly, Matthew. “Designing Reliable Controllers For Bipedal Robots .” 2016. Web. 25 Mar 2019.

Vancouver:

Kelly M. Designing Reliable Controllers For Bipedal Robots . [Internet] [Thesis]. Cornell University; 2016. [cited 2019 Mar 25]. Available from: http://hdl.handle.net/1813/44350.

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

Council of Science Editors:

Kelly M. Designing Reliable Controllers For Bipedal Robots . [Thesis]. Cornell University; 2016. Available from: http://hdl.handle.net/1813/44350

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


Linköping University

11. Stenström, Jonathan. Simultaneous Trajectory Optimization and Target Estimation Using RSS Measurements to Land a UAV.

Degree: Automatic Control, 2016, Linköping University

  The use of autonomous UAV’s is a progressively expanding industry. This thesisfocuses on the landing procedure with the main goal to be independent of… (more)

Subjects/Keywords: EKF RSS; UAV; Autonomous landing; Trajectory optimization

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APA (6th Edition):

Stenström, J. (2016). Simultaneous Trajectory Optimization and Target Estimation Using RSS Measurements to Land a UAV. (Thesis). Linköping University. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-131117

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):

Stenström, Jonathan. “Simultaneous Trajectory Optimization and Target Estimation Using RSS Measurements to Land a UAV.” 2016. Thesis, Linköping University. Accessed March 25, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-131117.

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

MLA Handbook (7th Edition):

Stenström, Jonathan. “Simultaneous Trajectory Optimization and Target Estimation Using RSS Measurements to Land a UAV.” 2016. Web. 25 Mar 2019.

Vancouver:

Stenström J. Simultaneous Trajectory Optimization and Target Estimation Using RSS Measurements to Land a UAV. [Internet] [Thesis]. Linköping University; 2016. [cited 2019 Mar 25]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-131117.

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

Council of Science Editors:

Stenström J. Simultaneous Trajectory Optimization and Target Estimation Using RSS Measurements to Land a UAV. [Thesis]. Linköping University; 2016. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-131117

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


Indian Institute of Science

12. Arora, Rajesh Kumar. Improved Solution Techniques For Trajectory Optimization With Application To A RLV-Demonstrator Mission.

Degree: 2006, Indian Institute of Science

 Solutions to trajectory optimization problems are carried out by the direct and indirect methods. Under broad heading of these methods, numerous algorithms such as collocation,… (more)

Subjects/Keywords: Genetic Algorithm; Spacecraft - Trajectory Optimization; Reusable Launch Vehicle (RLV); On-line Trajectory-Reshaping Algorithm; Trajectory Dispersion; Trajectory Optimization; Trajectory Design; Re-entry Vehicles; Chebyshev Polynomials; Astronautics

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

APA (6th Edition):

Arora, R. K. (2006). Improved Solution Techniques For Trajectory Optimization With Application To A RLV-Demonstrator Mission. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/424

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):

Arora, Rajesh Kumar. “Improved Solution Techniques For Trajectory Optimization With Application To A RLV-Demonstrator Mission.” 2006. Thesis, Indian Institute of Science. Accessed March 25, 2019. http://hdl.handle.net/2005/424.

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

MLA Handbook (7th Edition):

Arora, Rajesh Kumar. “Improved Solution Techniques For Trajectory Optimization With Application To A RLV-Demonstrator Mission.” 2006. Web. 25 Mar 2019.

Vancouver:

Arora RK. Improved Solution Techniques For Trajectory Optimization With Application To A RLV-Demonstrator Mission. [Internet] [Thesis]. Indian Institute of Science; 2006. [cited 2019 Mar 25]. Available from: http://hdl.handle.net/2005/424.

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

Council of Science Editors:

Arora RK. Improved Solution Techniques For Trajectory Optimization With Application To A RLV-Demonstrator Mission. [Thesis]. Indian Institute of Science; 2006. Available from: http://hdl.handle.net/2005/424

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


University of Minnesota

13. Tetzman, Derrick G. Simulation and optimization of spacecraft re-entry Trajectories.

Degree: 2010, University of Minnesota

University of Minnesota M.S. thesis. May 2010. Major: Aerospace Engineering and Mechanics. Advisors:Dr. William Garrard, Dr. Yiyuan Zhao. 1 computer file (PDF); x, 113 pages,… (more)

Subjects/Keywords: Trajectory optimization; Spacecraft; Control algorithm; Optimization program; Aerospace Engineering and Mechanics

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APA (6th Edition):

Tetzman, D. G. (2010). Simulation and optimization of spacecraft re-entry Trajectories. (Masters Thesis). University of Minnesota. Retrieved from http://purl.umn.edu/93005

Chicago Manual of Style (16th Edition):

Tetzman, Derrick G. “Simulation and optimization of spacecraft re-entry Trajectories.” 2010. Masters Thesis, University of Minnesota. Accessed March 25, 2019. http://purl.umn.edu/93005.

MLA Handbook (7th Edition):

Tetzman, Derrick G. “Simulation and optimization of spacecraft re-entry Trajectories.” 2010. Web. 25 Mar 2019.

Vancouver:

Tetzman DG. Simulation and optimization of spacecraft re-entry Trajectories. [Internet] [Masters thesis]. University of Minnesota; 2010. [cited 2019 Mar 25]. Available from: http://purl.umn.edu/93005.

Council of Science Editors:

Tetzman DG. Simulation and optimization of spacecraft re-entry Trajectories. [Masters Thesis]. University of Minnesota; 2010. Available from: http://purl.umn.edu/93005


University of Alberta

14. Kansal, Sachin. Trajectory optimization for flat dynamic systems.

Degree: MS, Department of Chemical and Materials Engineering, 2000, University of Alberta

Subjects/Keywords: Trajectory optimization.; Mathematical optimization.

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

APA (6th Edition):

Kansal, S. (2000). Trajectory optimization for flat dynamic systems. (Masters Thesis). University of Alberta. Retrieved from https://era.library.ualberta.ca/files/3j3334318

Chicago Manual of Style (16th Edition):

Kansal, Sachin. “Trajectory optimization for flat dynamic systems.” 2000. Masters Thesis, University of Alberta. Accessed March 25, 2019. https://era.library.ualberta.ca/files/3j3334318.

MLA Handbook (7th Edition):

Kansal, Sachin. “Trajectory optimization for flat dynamic systems.” 2000. Web. 25 Mar 2019.

Vancouver:

Kansal S. Trajectory optimization for flat dynamic systems. [Internet] [Masters thesis]. University of Alberta; 2000. [cited 2019 Mar 25]. Available from: https://era.library.ualberta.ca/files/3j3334318.

Council of Science Editors:

Kansal S. Trajectory optimization for flat dynamic systems. [Masters Thesis]. University of Alberta; 2000. Available from: https://era.library.ualberta.ca/files/3j3334318


Georgia Tech

15. Steffens, Michael J. A combined global and local methodology for launch vehicle trajectory design-space exploration and optimization.

Degree: MS, Aerospace Engineering, 2014, Georgia Tech

Trajectory optimization is an important part of launch vehicle design and operation. With the high costs of launching payload into orbit, every pound that can… (more)

Subjects/Keywords: Launch vehicle; Trajectory optimization; Launch vehicles (Astronautics); Trajectories (Mechanics); Mathematical optimization

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

APA (6th Edition):

Steffens, M. J. (2014). A combined global and local methodology for launch vehicle trajectory design-space exploration and optimization. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/51884

Chicago Manual of Style (16th Edition):

Steffens, Michael J. “A combined global and local methodology for launch vehicle trajectory design-space exploration and optimization.” 2014. Masters Thesis, Georgia Tech. Accessed March 25, 2019. http://hdl.handle.net/1853/51884.

MLA Handbook (7th Edition):

Steffens, Michael J. “A combined global and local methodology for launch vehicle trajectory design-space exploration and optimization.” 2014. Web. 25 Mar 2019.

Vancouver:

Steffens MJ. A combined global and local methodology for launch vehicle trajectory design-space exploration and optimization. [Internet] [Masters thesis]. Georgia Tech; 2014. [cited 2019 Mar 25]. Available from: http://hdl.handle.net/1853/51884.

Council of Science Editors:

Steffens MJ. A combined global and local methodology for launch vehicle trajectory design-space exploration and optimization. [Masters Thesis]. Georgia Tech; 2014. Available from: http://hdl.handle.net/1853/51884


University of Minnesota

16. Tetzman, Derrick G. Simulation and optimization of spacecraft re-entry Trajectories.

Degree: MS, Aerospace Engineering and Mechanics, 2010, University of Minnesota

 Parameter optimal control has the advantage of often being easier and faster to solve than general optimal control methods, and may be better suited to… (more)

Subjects/Keywords: Trajectory optimization; Spacecraft; Control algorithm; Optimization program; Aerospace Engineering and Mechanics

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APA (6th Edition):

Tetzman, D. G. (2010). Simulation and optimization of spacecraft re-entry Trajectories. (Masters Thesis). University of Minnesota. Retrieved from http://purl.umn.edu/93005

Chicago Manual of Style (16th Edition):

Tetzman, Derrick G. “Simulation and optimization of spacecraft re-entry Trajectories.” 2010. Masters Thesis, University of Minnesota. Accessed March 25, 2019. http://purl.umn.edu/93005.

MLA Handbook (7th Edition):

Tetzman, Derrick G. “Simulation and optimization of spacecraft re-entry Trajectories.” 2010. Web. 25 Mar 2019.

Vancouver:

Tetzman DG. Simulation and optimization of spacecraft re-entry Trajectories. [Internet] [Masters thesis]. University of Minnesota; 2010. [cited 2019 Mar 25]. Available from: http://purl.umn.edu/93005.

Council of Science Editors:

Tetzman DG. Simulation and optimization of spacecraft re-entry Trajectories. [Masters Thesis]. University of Minnesota; 2010. Available from: http://purl.umn.edu/93005


Iowa State University

17. Murillo, Oscar Jaime. A fast ascent trajectory optimization method for hypersonic air-breathing vehicles.

Degree: 2010, Iowa State University

 The objective of this dissertation is to investigate a fast and reliable method to generate three-dimensional optimal ascent trajectories for hypersonic air-breathing vehicles. The problem… (more)

Subjects/Keywords: Ascent Trajectory; Hypersonic Air-breathing vehicles; Hypersonic Ascent; Trajectory Optimization; Aerospace Engineering

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APA (6th Edition):

Murillo, O. J. (2010). A fast ascent trajectory optimization method for hypersonic air-breathing vehicles. (Thesis). Iowa State University. Retrieved from https://lib.dr.iastate.edu/etd/11825

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):

Murillo, Oscar Jaime. “A fast ascent trajectory optimization method for hypersonic air-breathing vehicles.” 2010. Thesis, Iowa State University. Accessed March 25, 2019. https://lib.dr.iastate.edu/etd/11825.

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

MLA Handbook (7th Edition):

Murillo, Oscar Jaime. “A fast ascent trajectory optimization method for hypersonic air-breathing vehicles.” 2010. Web. 25 Mar 2019.

Vancouver:

Murillo OJ. A fast ascent trajectory optimization method for hypersonic air-breathing vehicles. [Internet] [Thesis]. Iowa State University; 2010. [cited 2019 Mar 25]. Available from: https://lib.dr.iastate.edu/etd/11825.

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

Council of Science Editors:

Murillo OJ. A fast ascent trajectory optimization method for hypersonic air-breathing vehicles. [Thesis]. Iowa State University; 2010. Available from: https://lib.dr.iastate.edu/etd/11825

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


Purdue University

18. Pritchett, Robert E. Numerical methods for low-thrust trajectory optimization.

Degree: MSin Aeronautics and Astronautics, Aeronautics and Astronautics, 2016, Purdue University

  The spacecraft trajectory design process frequently includes the optimization of a quantity of importance such as propellant consumption or time of flight. A variety… (more)

Subjects/Keywords: Applied sciences; Collocation; Direct optimization; Indirect optimization; Low-thrust; Spacecraft trajectory optimization; Aerospace Engineering

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

APA (6th Edition):

Pritchett, R. E. (2016). Numerical methods for low-thrust trajectory optimization. (Thesis). Purdue University. Retrieved from https://docs.lib.purdue.edu/open_access_theses/986

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):

Pritchett, Robert E. “Numerical methods for low-thrust trajectory optimization.” 2016. Thesis, Purdue University. Accessed March 25, 2019. https://docs.lib.purdue.edu/open_access_theses/986.

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

MLA Handbook (7th Edition):

Pritchett, Robert E. “Numerical methods for low-thrust trajectory optimization.” 2016. Web. 25 Mar 2019.

Vancouver:

Pritchett RE. Numerical methods for low-thrust trajectory optimization. [Internet] [Thesis]. Purdue University; 2016. [cited 2019 Mar 25]. Available from: https://docs.lib.purdue.edu/open_access_theses/986.

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

Council of Science Editors:

Pritchett RE. Numerical methods for low-thrust trajectory optimization. [Thesis]. Purdue University; 2016. Available from: https://docs.lib.purdue.edu/open_access_theses/986

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


University of Waterloo

19. Tabandeh, Saleh. Development of Novel Task-Based Configuration Optimization Methodologies for Modular and Reconfigurable Robots Using Multi-Solution Inverse Kinematic Algorithms.

Degree: 2010, University of Waterloo

 Modular and Reconfigurable Robots (MRRs) are those designed to address the increasing demand for flexible and versatile manipulators in manufacturing facilities. The term, modularity, indicates… (more)

Subjects/Keywords: inverse kinematics; Modular Robotics; Genetic Algorithms; Optimization Algorithms; Task-Based Configuration Optimization; Trajectory Optimization

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APA (6th Edition):

Tabandeh, S. (2010). Development of Novel Task-Based Configuration Optimization Methodologies for Modular and Reconfigurable Robots Using Multi-Solution Inverse Kinematic Algorithms. (Thesis). University of Waterloo. Retrieved from http://hdl.handle.net/10012/4959

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):

Tabandeh, Saleh. “Development of Novel Task-Based Configuration Optimization Methodologies for Modular and Reconfigurable Robots Using Multi-Solution Inverse Kinematic Algorithms.” 2010. Thesis, University of Waterloo. Accessed March 25, 2019. http://hdl.handle.net/10012/4959.

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

MLA Handbook (7th Edition):

Tabandeh, Saleh. “Development of Novel Task-Based Configuration Optimization Methodologies for Modular and Reconfigurable Robots Using Multi-Solution Inverse Kinematic Algorithms.” 2010. Web. 25 Mar 2019.

Vancouver:

Tabandeh S. Development of Novel Task-Based Configuration Optimization Methodologies for Modular and Reconfigurable Robots Using Multi-Solution Inverse Kinematic Algorithms. [Internet] [Thesis]. University of Waterloo; 2010. [cited 2019 Mar 25]. Available from: http://hdl.handle.net/10012/4959.

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

Council of Science Editors:

Tabandeh S. Development of Novel Task-Based Configuration Optimization Methodologies for Modular and Reconfigurable Robots Using Multi-Solution Inverse Kinematic Algorithms. [Thesis]. University of Waterloo; 2010. Available from: http://hdl.handle.net/10012/4959

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


University of Illinois – Urbana-Champaign

20. Ghosh, Alexander. Multi-CubeSat mission planning enabled through parallel computing.

Degree: PhD, 4048, 2013, University of Illinois – Urbana-Champaign

 Small CubeSat-class satellites are opening up new avenues for science and technology development within the space industry. What was once a purely educational tool has… (more)

Subjects/Keywords: satellite; trajectory; trajectory optimization; optimization; cubesat; picosatellite; earth orbit; Orbit; low thrust; low-thrust; automatic differentiation; algorithmic differentiation; parallel processing

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

APA (6th Edition):

Ghosh, A. (2013). Multi-CubeSat mission planning enabled through parallel computing. (Doctoral Dissertation). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/45554

Chicago Manual of Style (16th Edition):

Ghosh, Alexander. “Multi-CubeSat mission planning enabled through parallel computing.” 2013. Doctoral Dissertation, University of Illinois – Urbana-Champaign. Accessed March 25, 2019. http://hdl.handle.net/2142/45554.

MLA Handbook (7th Edition):

Ghosh, Alexander. “Multi-CubeSat mission planning enabled through parallel computing.” 2013. Web. 25 Mar 2019.

Vancouver:

Ghosh A. Multi-CubeSat mission planning enabled through parallel computing. [Internet] [Doctoral dissertation]. University of Illinois – Urbana-Champaign; 2013. [cited 2019 Mar 25]. Available from: http://hdl.handle.net/2142/45554.

Council of Science Editors:

Ghosh A. Multi-CubeSat mission planning enabled through parallel computing. [Doctoral Dissertation]. University of Illinois – Urbana-Champaign; 2013. Available from: http://hdl.handle.net/2142/45554


University of Minnesota

21. Devulapalli, Raghuveer. An efficient algorithm for commercial aircraft trajectory optimization in the air traffic system.

Degree: MS, Aerospace Engineering and Mechanics, 2012, University of Minnesota

University of Minnesota M.S. thesis. July 2012. Major: Aerospace Engineering and Mechanics. Advisor: Yiyuan J. Zhao. 1 computer file (PDF); vii, 64 pages.

A discrete… (more)

Subjects/Keywords: A* algorithm; Commercial aircrafts; Discrete optimization; Flight planning; Trajectory Optimization; Wind optimal routing

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APA (6th Edition):

Devulapalli, R. (2012). An efficient algorithm for commercial aircraft trajectory optimization in the air traffic system. (Masters Thesis). University of Minnesota. Retrieved from http://purl.umn.edu/140007

Chicago Manual of Style (16th Edition):

Devulapalli, Raghuveer. “An efficient algorithm for commercial aircraft trajectory optimization in the air traffic system.” 2012. Masters Thesis, University of Minnesota. Accessed March 25, 2019. http://purl.umn.edu/140007.

MLA Handbook (7th Edition):

Devulapalli, Raghuveer. “An efficient algorithm for commercial aircraft trajectory optimization in the air traffic system.” 2012. Web. 25 Mar 2019.

Vancouver:

Devulapalli R. An efficient algorithm for commercial aircraft trajectory optimization in the air traffic system. [Internet] [Masters thesis]. University of Minnesota; 2012. [cited 2019 Mar 25]. Available from: http://purl.umn.edu/140007.

Council of Science Editors:

Devulapalli R. An efficient algorithm for commercial aircraft trajectory optimization in the air traffic system. [Masters Thesis]. University of Minnesota; 2012. Available from: http://purl.umn.edu/140007


University of Colorado

22. Feldhacker, Juliana D. Incorporating Uncertainty into Spacecraft Mission and Trajectory Design.

Degree: PhD, Aerospace Engineering Sciences, 2016, University of Colorado

  The complex nature of many astrodynamic systems often leads to high computational costs or degraded accuracy in the analysis and design of spacecraft missions,… (more)

Subjects/Keywords: mission design; optimization under uncertainty; robust design; trajectory optimization; uncertainty quantification; Aerospace Engineering

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APA (6th Edition):

Feldhacker, J. D. (2016). Incorporating Uncertainty into Spacecraft Mission and Trajectory Design. (Doctoral Dissertation). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/135

Chicago Manual of Style (16th Edition):

Feldhacker, Juliana D. “Incorporating Uncertainty into Spacecraft Mission and Trajectory Design.” 2016. Doctoral Dissertation, University of Colorado. Accessed March 25, 2019. http://scholar.colorado.edu/asen_gradetds/135.

MLA Handbook (7th Edition):

Feldhacker, Juliana D. “Incorporating Uncertainty into Spacecraft Mission and Trajectory Design.” 2016. Web. 25 Mar 2019.

Vancouver:

Feldhacker JD. Incorporating Uncertainty into Spacecraft Mission and Trajectory Design. [Internet] [Doctoral dissertation]. University of Colorado; 2016. [cited 2019 Mar 25]. Available from: http://scholar.colorado.edu/asen_gradetds/135.

Council of Science Editors:

Feldhacker JD. Incorporating Uncertainty into Spacecraft Mission and Trajectory Design. [Doctoral Dissertation]. University of Colorado; 2016. Available from: http://scholar.colorado.edu/asen_gradetds/135


Georgia Tech

23. Moore, Roxanne Adele. Variable fidelity modeling as applied to trajectory optimization for a hydraulic backhoe.

Degree: MS, Mechanical Engineering, 2009, Georgia Tech

 Modeling, simulation, and optimization play vital roles throughout the engineering design process; however, in many design disciplines the cost of simulation is high, and designers… (more)

Subjects/Keywords: Modeling; Variable-fidelity; Simulation; Optimization; Backhoe; Fluid power; Hydrualics; Backhoes; Trajectory optimization

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

APA (6th Edition):

Moore, R. A. (2009). Variable fidelity modeling as applied to trajectory optimization for a hydraulic backhoe. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/28146

Chicago Manual of Style (16th Edition):

Moore, Roxanne Adele. “Variable fidelity modeling as applied to trajectory optimization for a hydraulic backhoe.” 2009. Masters Thesis, Georgia Tech. Accessed March 25, 2019. http://hdl.handle.net/1853/28146.

MLA Handbook (7th Edition):

Moore, Roxanne Adele. “Variable fidelity modeling as applied to trajectory optimization for a hydraulic backhoe.” 2009. Web. 25 Mar 2019.

Vancouver:

Moore RA. Variable fidelity modeling as applied to trajectory optimization for a hydraulic backhoe. [Internet] [Masters thesis]. Georgia Tech; 2009. [cited 2019 Mar 25]. Available from: http://hdl.handle.net/1853/28146.

Council of Science Editors:

Moore RA. Variable fidelity modeling as applied to trajectory optimization for a hydraulic backhoe. [Masters Thesis]. Georgia Tech; 2009. Available from: http://hdl.handle.net/1853/28146


University of Texas – Austin

24. Jesick, Mark Christopher. Optimal lunar orbit insertion from a free return trajectory.

Degree: Aerospace Engineering, 2012, University of Texas – Austin

 With the discovery of water ice at the moon's south pole, future human lunar exploration will likely occur at polar sites and, therefore, require high… (more)

Subjects/Keywords: Free return; Trajectory optimization; Lunar orbit insertion; Mission design; Parameter optimization; Optimal control theory

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APA (6th Edition):

Jesick, M. C. (2012). Optimal lunar orbit insertion from a free return trajectory. (Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/32893

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):

Jesick, Mark Christopher. “Optimal lunar orbit insertion from a free return trajectory.” 2012. Thesis, University of Texas – Austin. Accessed March 25, 2019. http://hdl.handle.net/2152/32893.

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

MLA Handbook (7th Edition):

Jesick, Mark Christopher. “Optimal lunar orbit insertion from a free return trajectory.” 2012. Web. 25 Mar 2019.

Vancouver:

Jesick MC. Optimal lunar orbit insertion from a free return trajectory. [Internet] [Thesis]. University of Texas – Austin; 2012. [cited 2019 Mar 25]. Available from: http://hdl.handle.net/2152/32893.

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

Council of Science Editors:

Jesick MC. Optimal lunar orbit insertion from a free return trajectory. [Thesis]. University of Texas – Austin; 2012. Available from: http://hdl.handle.net/2152/32893

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


University of Texas – Austin

25. Campbell, Alan Robert. Numerical analysis of complex-step differentiation in spacecraft trajectory optimization problems.

Degree: Aerospace Engineering, 2011, University of Texas – Austin

 An analysis of the use of complex-step differentiation (CSD) in optimization problems is presented. Complex-step differentiation is a numerical approximation of the derivative of a… (more)

Subjects/Keywords: Trajectory optimization; Numerical differentiation; Complex step differentiation; Optimization; Lunar ascent problem; Optimal orbit transfer problem

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APA (6th Edition):

Campbell, A. R. (2011). Numerical analysis of complex-step differentiation in spacecraft trajectory optimization problems. (Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/ETD-UT-2011-05-3440

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):

Campbell, Alan Robert. “Numerical analysis of complex-step differentiation in spacecraft trajectory optimization problems.” 2011. Thesis, University of Texas – Austin. Accessed March 25, 2019. http://hdl.handle.net/2152/ETD-UT-2011-05-3440.

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

MLA Handbook (7th Edition):

Campbell, Alan Robert. “Numerical analysis of complex-step differentiation in spacecraft trajectory optimization problems.” 2011. Web. 25 Mar 2019.

Vancouver:

Campbell AR. Numerical analysis of complex-step differentiation in spacecraft trajectory optimization problems. [Internet] [Thesis]. University of Texas – Austin; 2011. [cited 2019 Mar 25]. Available from: http://hdl.handle.net/2152/ETD-UT-2011-05-3440.

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

Council of Science Editors:

Campbell AR. Numerical analysis of complex-step differentiation in spacecraft trajectory optimization problems. [Thesis]. University of Texas – Austin; 2011. Available from: http://hdl.handle.net/2152/ETD-UT-2011-05-3440

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


University of Minnesota

26. Devulapalli, Raghuveer. An efficient algorithm for commercial aircraft trajectory optimization in the air traffic system.

Degree: MS, Aerospace Engineering and Mechanics, 2012, University of Minnesota

 A discrete search strategy is presented to determine optimal aircraft trajectories which can be unconstrained or regulated to follow current Air Traffic Control (ATC) procedures.… (more)

Subjects/Keywords: A* algorithm; Commercial aircrafts; Discrete optimization; Flight planning; Trajectory Optimization; Wind optimal routing

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

APA (6th Edition):

Devulapalli, R. (2012). An efficient algorithm for commercial aircraft trajectory optimization in the air traffic system. (Masters Thesis). University of Minnesota. Retrieved from http://purl.umn.edu/140007

Chicago Manual of Style (16th Edition):

Devulapalli, Raghuveer. “An efficient algorithm for commercial aircraft trajectory optimization in the air traffic system.” 2012. Masters Thesis, University of Minnesota. Accessed March 25, 2019. http://purl.umn.edu/140007.

MLA Handbook (7th Edition):

Devulapalli, Raghuveer. “An efficient algorithm for commercial aircraft trajectory optimization in the air traffic system.” 2012. Web. 25 Mar 2019.

Vancouver:

Devulapalli R. An efficient algorithm for commercial aircraft trajectory optimization in the air traffic system. [Internet] [Masters thesis]. University of Minnesota; 2012. [cited 2019 Mar 25]. Available from: http://purl.umn.edu/140007.

Council of Science Editors:

Devulapalli R. An efficient algorithm for commercial aircraft trajectory optimization in the air traffic system. [Masters Thesis]. University of Minnesota; 2012. Available from: http://purl.umn.edu/140007


Georgia Tech

27. De La Torre, Gerardo. Autonomous suspended load operations via trajectory optimization and variational integrators.

Degree: PhD, Aerospace Engineering, 2015, Georgia Tech

 Advances in machine autonomy hold great promise in advancing technology, economic markets, and general societal well-being. For example, the progression of unmanned air systems (UAS)… (more)

Subjects/Keywords: Trajectory optimization; Variational integrator; Suspended load; Stochastic control; Polynomial chaos

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APA (6th Edition):

De La Torre, G. (2015). Autonomous suspended load operations via trajectory optimization and variational integrators. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/53932

Chicago Manual of Style (16th Edition):

De La Torre, Gerardo. “Autonomous suspended load operations via trajectory optimization and variational integrators.” 2015. Doctoral Dissertation, Georgia Tech. Accessed March 25, 2019. http://hdl.handle.net/1853/53932.

MLA Handbook (7th Edition):

De La Torre, Gerardo. “Autonomous suspended load operations via trajectory optimization and variational integrators.” 2015. Web. 25 Mar 2019.

Vancouver:

De La Torre G. Autonomous suspended load operations via trajectory optimization and variational integrators. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2019 Mar 25]. Available from: http://hdl.handle.net/1853/53932.

Council of Science Editors:

De La Torre G. Autonomous suspended load operations via trajectory optimization and variational integrators. [Doctoral Dissertation]. Georgia Tech; 2015. Available from: http://hdl.handle.net/1853/53932


Purdue University

28. Williams, Joseph. Trajectory optimization using indirect methods and parametric scramjet cycle analysis.

Degree: MSin Aeronautics and Astronautics, Aeronautics and Astronautics, 2016, Purdue University

  This study investigates the solution of time sensitive regional strike trajectories for hypersonic missiles. This minimum time trajectory is suspected to be best performed… (more)

Subjects/Keywords: Applied sciences; Indirect; Optimization; Powered; Regularization; Scramjet; Trajectory; Aerospace Engineering

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APA (6th Edition):

Williams, J. (2016). Trajectory optimization using indirect methods and parametric scramjet cycle analysis. (Thesis). Purdue University. Retrieved from https://docs.lib.purdue.edu/open_access_theses/908

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):

Williams, Joseph. “Trajectory optimization using indirect methods and parametric scramjet cycle analysis.” 2016. Thesis, Purdue University. Accessed March 25, 2019. https://docs.lib.purdue.edu/open_access_theses/908.

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

MLA Handbook (7th Edition):

Williams, Joseph. “Trajectory optimization using indirect methods and parametric scramjet cycle analysis.” 2016. Web. 25 Mar 2019.

Vancouver:

Williams J. Trajectory optimization using indirect methods and parametric scramjet cycle analysis. [Internet] [Thesis]. Purdue University; 2016. [cited 2019 Mar 25]. Available from: https://docs.lib.purdue.edu/open_access_theses/908.

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

Council of Science Editors:

Williams J. Trajectory optimization using indirect methods and parametric scramjet cycle analysis. [Thesis]. Purdue University; 2016. Available from: https://docs.lib.purdue.edu/open_access_theses/908

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


Hong Kong University of Science and Technology

29. Liu, Xiaoying. Trajectory data compression via spatial-temporal properties.

Degree: 2014, Hong Kong University of Science and Technology

 User movement can be captured using devices such as mobile phones, GPS trackers and smart RFID cards. The popularity of these devices has led to… (more)

Subjects/Keywords: Global Positioning System; Data processing; Mathematical models; Trajectory optimization

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APA (6th Edition):

Liu, X. (2014). Trajectory data compression via spatial-temporal properties. (Thesis). Hong Kong University of Science and Technology. Retrieved from https://doi.org/10.14711/thesis-b1301528 ; http://repository.ust.hk/ir/bitstream/1783.1-73427/1/th_redirect.html

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):

Liu, Xiaoying. “Trajectory data compression via spatial-temporal properties.” 2014. Thesis, Hong Kong University of Science and Technology. Accessed March 25, 2019. https://doi.org/10.14711/thesis-b1301528 ; http://repository.ust.hk/ir/bitstream/1783.1-73427/1/th_redirect.html.

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

MLA Handbook (7th Edition):

Liu, Xiaoying. “Trajectory data compression via spatial-temporal properties.” 2014. Web. 25 Mar 2019.

Vancouver:

Liu X. Trajectory data compression via spatial-temporal properties. [Internet] [Thesis]. Hong Kong University of Science and Technology; 2014. [cited 2019 Mar 25]. Available from: https://doi.org/10.14711/thesis-b1301528 ; http://repository.ust.hk/ir/bitstream/1783.1-73427/1/th_redirect.html.

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

Council of Science Editors:

Liu X. Trajectory data compression via spatial-temporal properties. [Thesis]. Hong Kong University of Science and Technology; 2014. Available from: https://doi.org/10.14711/thesis-b1301528 ; http://repository.ust.hk/ir/bitstream/1783.1-73427/1/th_redirect.html

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


Hong Kong University of Science and Technology

30. Lu, Lu. Visualization of map-matching for vehicle trajectories.

Degree: 2011, Hong Kong University of Science and Technology

 For vehicles equipped with GPS devices, their recorded trajectories are often erroneous or at least inaccurate. Thus, trajectory enhancement is required for applications that need… (more)

Subjects/Keywords: Global Positioning System  – Data processing; Trajectory optimization; Matching theory

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APA (6th Edition):

Lu, L. (2011). Visualization of map-matching for vehicle trajectories. (Thesis). Hong Kong University of Science and Technology. Retrieved from https://doi.org/10.14711/thesis-b1154803 ; http://repository.ust.hk/ir/bitstream/1783.1-7389/1/th_redirect.html

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):

Lu, Lu. “Visualization of map-matching for vehicle trajectories.” 2011. Thesis, Hong Kong University of Science and Technology. Accessed March 25, 2019. https://doi.org/10.14711/thesis-b1154803 ; http://repository.ust.hk/ir/bitstream/1783.1-7389/1/th_redirect.html.

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

MLA Handbook (7th Edition):

Lu, Lu. “Visualization of map-matching for vehicle trajectories.” 2011. Web. 25 Mar 2019.

Vancouver:

Lu L. Visualization of map-matching for vehicle trajectories. [Internet] [Thesis]. Hong Kong University of Science and Technology; 2011. [cited 2019 Mar 25]. Available from: https://doi.org/10.14711/thesis-b1154803 ; http://repository.ust.hk/ir/bitstream/1783.1-7389/1/th_redirect.html.

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

Council of Science Editors:

Lu L. Visualization of map-matching for vehicle trajectories. [Thesis]. Hong Kong University of Science and Technology; 2011. Available from: https://doi.org/10.14711/thesis-b1154803 ; http://repository.ust.hk/ir/bitstream/1783.1-7389/1/th_redirect.html

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

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