Advanced search options

Advanced Search Options 🞨

Browse by author name (“Author name starts with…”).

Find ETDs with:

in
/  
in
/  
in
/  
in

Written in Published in Earliest date Latest date

Sorted by

Results per page:

Sorted by: relevance · author · university · dateNew search

You searched for subject:(Three body problem ). Showing records 1 – 30 of 25389 total matches.

[1] [2] [3] [4] [5] … [847]

Search Limiters

Last 2 Years | English Only

Degrees

Languages

Country

▼ Search Limiters


University of Georgia

1. Hannah, Mark Edward. An analysis of the three body problem.

Degree: 2014, University of Georgia

 In this paper we will be presenting my approach to generating two possible solutions to the three-body problem. We will first discuss the theory of… (more)

Subjects/Keywords: Celestial Mechanics; n-Body Problem; Three-body Problem; 3-Body Problem

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Hannah, M. E. (2014). An analysis of the three body problem. (Thesis). University of Georgia. Retrieved from http://hdl.handle.net/10724/29188

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):

Hannah, Mark Edward. “An analysis of the three body problem.” 2014. Thesis, University of Georgia. Accessed October 30, 2020. http://hdl.handle.net/10724/29188.

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

MLA Handbook (7th Edition):

Hannah, Mark Edward. “An analysis of the three body problem.” 2014. Web. 30 Oct 2020.

Vancouver:

Hannah ME. An analysis of the three body problem. [Internet] [Thesis]. University of Georgia; 2014. [cited 2020 Oct 30]. Available from: http://hdl.handle.net/10724/29188.

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

Council of Science Editors:

Hannah ME. An analysis of the three body problem. [Thesis]. University of Georgia; 2014. Available from: http://hdl.handle.net/10724/29188

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


University of Johannesburg

2. Anderson, Keegan Doig. Gravitational capture.

Degree: 2012, University of Johannesburg

M.Sc.

Important ideas from dynamical systems theory and the restricted three-body problem are introduced. The intention is the application of dynamical systems theory techniques to… (more)

Subjects/Keywords: Gravitation; Space trajectories; Dynamics; Three-body problem; Two-body problem

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Anderson, K. D. (2012). Gravitational capture. (Thesis). University of Johannesburg. Retrieved from http://hdl.handle.net/10210/8053

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):

Anderson, Keegan Doig. “Gravitational capture.” 2012. Thesis, University of Johannesburg. Accessed October 30, 2020. http://hdl.handle.net/10210/8053.

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

MLA Handbook (7th Edition):

Anderson, Keegan Doig. “Gravitational capture.” 2012. Web. 30 Oct 2020.

Vancouver:

Anderson KD. Gravitational capture. [Internet] [Thesis]. University of Johannesburg; 2012. [cited 2020 Oct 30]. Available from: http://hdl.handle.net/10210/8053.

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

Council of Science Editors:

Anderson KD. Gravitational capture. [Thesis]. University of Johannesburg; 2012. Available from: http://hdl.handle.net/10210/8053

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


University of British Columbia

3. Hamilton, Rognvald Thore. The limiting case of periodic orbits near the lagrangian equilateral triangle solutions of the restricted three body problem.

Degree: MA- MA, Mathematics, 1939, University of British Columbia

[No abstract available]

Subjects/Keywords: Three-body problem

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Hamilton, R. T. (1939). The limiting case of periodic orbits near the lagrangian equilateral triangle solutions of the restricted three body problem. (Masters Thesis). University of British Columbia. Retrieved from http://hdl.handle.net/2429/38714

Chicago Manual of Style (16th Edition):

Hamilton, Rognvald Thore. “The limiting case of periodic orbits near the lagrangian equilateral triangle solutions of the restricted three body problem.” 1939. Masters Thesis, University of British Columbia. Accessed October 30, 2020. http://hdl.handle.net/2429/38714.

MLA Handbook (7th Edition):

Hamilton, Rognvald Thore. “The limiting case of periodic orbits near the lagrangian equilateral triangle solutions of the restricted three body problem.” 1939. Web. 30 Oct 2020.

Vancouver:

Hamilton RT. The limiting case of periodic orbits near the lagrangian equilateral triangle solutions of the restricted three body problem. [Internet] [Masters thesis]. University of British Columbia; 1939. [cited 2020 Oct 30]. Available from: http://hdl.handle.net/2429/38714.

Council of Science Editors:

Hamilton RT. The limiting case of periodic orbits near the lagrangian equilateral triangle solutions of the restricted three body problem. [Masters Thesis]. University of British Columbia; 1939. Available from: http://hdl.handle.net/2429/38714


The Ohio State University

4. Jedrey, Richard M. Development of a Discretized Model for the Restricted Three-Body Problem.

Degree: MS, Aero/Astro Engineering, 2011, The Ohio State University

 Spacecraft trajectory design is a science that requires high precision with little error. One of the most classic trajectory design problems is the restricted three-body(more)

Subjects/Keywords: Aerospace Engineering; Engineering; orbital mechanics; spacecraft trajectories; three-body problem; three-body model; n-body problem; n-body model; discretized spacecraft

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Jedrey, R. M. (2011). Development of a Discretized Model for the Restricted Three-Body Problem. (Masters Thesis). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1306856595

Chicago Manual of Style (16th Edition):

Jedrey, Richard M. “Development of a Discretized Model for the Restricted Three-Body Problem.” 2011. Masters Thesis, The Ohio State University. Accessed October 30, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=osu1306856595.

MLA Handbook (7th Edition):

Jedrey, Richard M. “Development of a Discretized Model for the Restricted Three-Body Problem.” 2011. Web. 30 Oct 2020.

Vancouver:

Jedrey RM. Development of a Discretized Model for the Restricted Three-Body Problem. [Internet] [Masters thesis]. The Ohio State University; 2011. [cited 2020 Oct 30]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1306856595.

Council of Science Editors:

Jedrey RM. Development of a Discretized Model for the Restricted Three-Body Problem. [Masters Thesis]. The Ohio State University; 2011. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1306856595


University of British Columbia

5. Barkham, Peter George Douglas. Some aspects of three and four-body dynamics.

Degree: PhD, Electrical and Computer Engineering, 1974, University of British Columbia

 Two fundamental problems of celestial mechanics are considered: the stellar or planetary three-body problem and a related form of the restricted four-body problem. Although a… (more)

Subjects/Keywords: Two-body problem; Three-body problem

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Barkham, P. G. D. (1974). Some aspects of three and four-body dynamics. (Doctoral Dissertation). University of British Columbia. Retrieved from http://hdl.handle.net/2429/18937

Chicago Manual of Style (16th Edition):

Barkham, Peter George Douglas. “Some aspects of three and four-body dynamics.” 1974. Doctoral Dissertation, University of British Columbia. Accessed October 30, 2020. http://hdl.handle.net/2429/18937.

MLA Handbook (7th Edition):

Barkham, Peter George Douglas. “Some aspects of three and four-body dynamics.” 1974. Web. 30 Oct 2020.

Vancouver:

Barkham PGD. Some aspects of three and four-body dynamics. [Internet] [Doctoral dissertation]. University of British Columbia; 1974. [cited 2020 Oct 30]. Available from: http://hdl.handle.net/2429/18937.

Council of Science Editors:

Barkham PGD. Some aspects of three and four-body dynamics. [Doctoral Dissertation]. University of British Columbia; 1974. Available from: http://hdl.handle.net/2429/18937


Texas A&M University

6. Kim, Hyerim. Advanced Mission Design: Interplanetary Super Highway Trajectory Method.

Degree: PhD, Aerospace Engineering, 2015, Texas A&M University

 Near-future space missions demand the delivery of massive payloads to deep space destinations. Given foreseeable propulsion technology, this is feasible only if we can design… (more)

Subjects/Keywords: low thrust trajectory; interplanetary super highway; three body problem

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Kim, H. (2015). Advanced Mission Design: Interplanetary Super Highway Trajectory Method. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/155436

Chicago Manual of Style (16th Edition):

Kim, Hyerim. “Advanced Mission Design: Interplanetary Super Highway Trajectory Method.” 2015. Doctoral Dissertation, Texas A&M University. Accessed October 30, 2020. http://hdl.handle.net/1969.1/155436.

MLA Handbook (7th Edition):

Kim, Hyerim. “Advanced Mission Design: Interplanetary Super Highway Trajectory Method.” 2015. Web. 30 Oct 2020.

Vancouver:

Kim H. Advanced Mission Design: Interplanetary Super Highway Trajectory Method. [Internet] [Doctoral dissertation]. Texas A&M University; 2015. [cited 2020 Oct 30]. Available from: http://hdl.handle.net/1969.1/155436.

Council of Science Editors:

Kim H. Advanced Mission Design: Interplanetary Super Highway Trajectory Method. [Doctoral Dissertation]. Texas A&M University; 2015. Available from: http://hdl.handle.net/1969.1/155436


Michigan State University

7. Larson, Nancy Marie Zander, 1946-. Three-body problem : a formalism and computer code for arbitrary kinds of particles.

Degree: PhD, Department of Physics, 1972, Michigan State University

Subjects/Keywords: Three-body problem; Nuclear physics

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Larson, Nancy Marie Zander, 1. (1972). Three-body problem : a formalism and computer code for arbitrary kinds of particles. (Doctoral Dissertation). Michigan State University. Retrieved from http://etd.lib.msu.edu/islandora/object/etd:18893

Chicago Manual of Style (16th Edition):

Larson, Nancy Marie Zander, 1946-. “Three-body problem : a formalism and computer code for arbitrary kinds of particles.” 1972. Doctoral Dissertation, Michigan State University. Accessed October 30, 2020. http://etd.lib.msu.edu/islandora/object/etd:18893.

MLA Handbook (7th Edition):

Larson, Nancy Marie Zander, 1946-. “Three-body problem : a formalism and computer code for arbitrary kinds of particles.” 1972. Web. 30 Oct 2020.

Vancouver:

Larson, Nancy Marie Zander 1. Three-body problem : a formalism and computer code for arbitrary kinds of particles. [Internet] [Doctoral dissertation]. Michigan State University; 1972. [cited 2020 Oct 30]. Available from: http://etd.lib.msu.edu/islandora/object/etd:18893.

Council of Science Editors:

Larson, Nancy Marie Zander 1. Three-body problem : a formalism and computer code for arbitrary kinds of particles. [Doctoral Dissertation]. Michigan State University; 1972. Available from: http://etd.lib.msu.edu/islandora/object/etd:18893


Boston University

8. Atanasova, Diana. Transit orbits and long-term dynamics in the near-parabolic restricted three-body problems.

Degree: PhD, Mathematics & Statistics, 2020, Boston University

 In this thesis, we consider the planar parabolic, hyperbolic, and highly-elliptic restricted three-body problems (R3BP). In particular, we formulate sufficient conditions for no transit (escape… (more)

Subjects/Keywords: Mathematics; Annulus map; Parabolic restricted three-body problem; Transit orbits

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Atanasova, D. (2020). Transit orbits and long-term dynamics in the near-parabolic restricted three-body problems. (Doctoral Dissertation). Boston University. Retrieved from http://hdl.handle.net/2144/39615

Chicago Manual of Style (16th Edition):

Atanasova, Diana. “Transit orbits and long-term dynamics in the near-parabolic restricted three-body problems.” 2020. Doctoral Dissertation, Boston University. Accessed October 30, 2020. http://hdl.handle.net/2144/39615.

MLA Handbook (7th Edition):

Atanasova, Diana. “Transit orbits and long-term dynamics in the near-parabolic restricted three-body problems.” 2020. Web. 30 Oct 2020.

Vancouver:

Atanasova D. Transit orbits and long-term dynamics in the near-parabolic restricted three-body problems. [Internet] [Doctoral dissertation]. Boston University; 2020. [cited 2020 Oct 30]. Available from: http://hdl.handle.net/2144/39615.

Council of Science Editors:

Atanasova D. Transit orbits and long-term dynamics in the near-parabolic restricted three-body problems. [Doctoral Dissertation]. Boston University; 2020. Available from: http://hdl.handle.net/2144/39615


Rutgers University

9. Trim, Nkosi Nathan. Visualizing solutions of the circular restricted three-body problem.

Degree: MS, Mathematical Sciences, 2009, Rutgers University

 The stability of a satellite near the Lagrange points is studied in a Circular Restricted Three-Body Problem (CR3BP). The Runge Kutta method is used to… (more)

Subjects/Keywords: Three-body problem; Celestial mechanics

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Trim, N. N. (2009). Visualizing solutions of the circular restricted three-body problem. (Masters Thesis). Rutgers University. Retrieved from http://hdl.rutgers.edu/1782.2/rucore10005600001.ETD.000051338

Chicago Manual of Style (16th Edition):

Trim, Nkosi Nathan. “Visualizing solutions of the circular restricted three-body problem.” 2009. Masters Thesis, Rutgers University. Accessed October 30, 2020. http://hdl.rutgers.edu/1782.2/rucore10005600001.ETD.000051338.

MLA Handbook (7th Edition):

Trim, Nkosi Nathan. “Visualizing solutions of the circular restricted three-body problem.” 2009. Web. 30 Oct 2020.

Vancouver:

Trim NN. Visualizing solutions of the circular restricted three-body problem. [Internet] [Masters thesis]. Rutgers University; 2009. [cited 2020 Oct 30]. Available from: http://hdl.rutgers.edu/1782.2/rucore10005600001.ETD.000051338.

Council of Science Editors:

Trim NN. Visualizing solutions of the circular restricted three-body problem. [Masters Thesis]. Rutgers University; 2009. Available from: http://hdl.rutgers.edu/1782.2/rucore10005600001.ETD.000051338


University of British Columbia

10. Banville, Marcel Roland. A variational wave function for the ground state of He³, and its application to the D(p,y)He³ capture reaction.

Degree: PhD, Physics, 1965, University of British Columbia

 The present work proposes trial wave functions for the three-body problem in nuclear physics taking into account the group theoretical classification of the states given… (more)

Subjects/Keywords: Helium  – Isotopes; Three-body problem

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Banville, M. R. (1965). A variational wave function for the ground state of He³, and its application to the D(p,y)He³ capture reaction. (Doctoral Dissertation). University of British Columbia. Retrieved from http://hdl.handle.net/2429/38375

Chicago Manual of Style (16th Edition):

Banville, Marcel Roland. “A variational wave function for the ground state of He³, and its application to the D(p,y)He³ capture reaction.” 1965. Doctoral Dissertation, University of British Columbia. Accessed October 30, 2020. http://hdl.handle.net/2429/38375.

MLA Handbook (7th Edition):

Banville, Marcel Roland. “A variational wave function for the ground state of He³, and its application to the D(p,y)He³ capture reaction.” 1965. Web. 30 Oct 2020.

Vancouver:

Banville MR. A variational wave function for the ground state of He³, and its application to the D(p,y)He³ capture reaction. [Internet] [Doctoral dissertation]. University of British Columbia; 1965. [cited 2020 Oct 30]. Available from: http://hdl.handle.net/2429/38375.

Council of Science Editors:

Banville MR. A variational wave function for the ground state of He³, and its application to the D(p,y)He³ capture reaction. [Doctoral Dissertation]. University of British Columbia; 1965. Available from: http://hdl.handle.net/2429/38375


Purdue University

11. Cox, Andrew D. Transfers to a gravitational saddle point: An extended mission design option for LISA Pathfinder.

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

  Any possible LISA Pathfinder extended mission will immediately follow the primary mission after completion of scientific observations and technical demonstrations in a Sun-Earth L1… (more)

Subjects/Keywords: Applied sciences; Bicircular restricted four-body problem; Circular restricted three-body problem; Design; LISA Pathfinder; Space; Trajectory; Aerospace Engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Cox, A. D. (2016). Transfers to a gravitational saddle point: An extended mission design option for LISA Pathfinder. (Thesis). Purdue University. Retrieved from http://docs.lib.purdue.edu/open_access_theses/762

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):

Cox, Andrew D. “Transfers to a gravitational saddle point: An extended mission design option for LISA Pathfinder.” 2016. Thesis, Purdue University. Accessed October 30, 2020. http://docs.lib.purdue.edu/open_access_theses/762.

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

MLA Handbook (7th Edition):

Cox, Andrew D. “Transfers to a gravitational saddle point: An extended mission design option for LISA Pathfinder.” 2016. Web. 30 Oct 2020.

Vancouver:

Cox AD. Transfers to a gravitational saddle point: An extended mission design option for LISA Pathfinder. [Internet] [Thesis]. Purdue University; 2016. [cited 2020 Oct 30]. Available from: http://docs.lib.purdue.edu/open_access_theses/762.

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

Council of Science Editors:

Cox AD. Transfers to a gravitational saddle point: An extended mission design option for LISA Pathfinder. [Thesis]. Purdue University; 2016. Available from: http://docs.lib.purdue.edu/open_access_theses/762

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


Delft University of Technology

12. Bonasera, Stefano (author). On lunar collision orbits: New methodologies for Moon-to-Moon transfer design.

Degree: 2017, Delft University of Technology

 Many interplanetary missions massively leverage the lunar gravitational pull in the so-called low-energy regime to converge to their aim, saving consistent amount of fuel. Among… (more)

Subjects/Keywords: Moon-to-Moon transfer; Circular restricted three-body problem; Bicircular restricted four-body problem; Collision orbits; Levi Civita regularization; Poincaré map

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Bonasera, S. (. (2017). On lunar collision orbits: New methodologies for Moon-to-Moon transfer design. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:3df3ef2f-efcc-429d-b204-e0cbba196ef5

Chicago Manual of Style (16th Edition):

Bonasera, Stefano (author). “On lunar collision orbits: New methodologies for Moon-to-Moon transfer design.” 2017. Masters Thesis, Delft University of Technology. Accessed October 30, 2020. http://resolver.tudelft.nl/uuid:3df3ef2f-efcc-429d-b204-e0cbba196ef5.

MLA Handbook (7th Edition):

Bonasera, Stefano (author). “On lunar collision orbits: New methodologies for Moon-to-Moon transfer design.” 2017. Web. 30 Oct 2020.

Vancouver:

Bonasera S(. On lunar collision orbits: New methodologies for Moon-to-Moon transfer design. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2020 Oct 30]. Available from: http://resolver.tudelft.nl/uuid:3df3ef2f-efcc-429d-b204-e0cbba196ef5.

Council of Science Editors:

Bonasera S(. On lunar collision orbits: New methodologies for Moon-to-Moon transfer design. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:3df3ef2f-efcc-429d-b204-e0cbba196ef5


Brno University of Technology

13. Bahník, Michal. Základy pohybu vesmírných těles: Basics of space motion.

Degree: 2019, Brno University of Technology

 This Bachelor thesis is a summarising text which deals with the issue of space motion. We analyse one-body, two-body and three-body problems. We derive analytical… (more)

Subjects/Keywords: Pohyb vesmírných těles; Kepler; probém dvou těles; problém tří těles; Space motion; Kepler; two-body problem; three-body problem

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Bahník, M. (2019). Základy pohybu vesmírných těles: Basics of space motion. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/26440

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):

Bahník, Michal. “Základy pohybu vesmírných těles: Basics of space motion.” 2019. Thesis, Brno University of Technology. Accessed October 30, 2020. http://hdl.handle.net/11012/26440.

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

MLA Handbook (7th Edition):

Bahník, Michal. “Základy pohybu vesmírných těles: Basics of space motion.” 2019. Web. 30 Oct 2020.

Vancouver:

Bahník M. Základy pohybu vesmírných těles: Basics of space motion. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2020 Oct 30]. Available from: http://hdl.handle.net/11012/26440.

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

Council of Science Editors:

Bahník M. Základy pohybu vesmírných těles: Basics of space motion. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/26440

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

14. Suryawanshi, Jay Shriram. Periodic Orbit Analytic Construction In The Circular Restricted Three-Body Problem.

Degree: MS, Mechanical & Aerospace Engineering, 2019, Old Dominion University

  This thesis investigates an approximate analytic construction of halo-type periodic orbits about the collinear equilibrium points in the circular restricted three-body problem. The research… (more)

Subjects/Keywords: Analytic construction; Halo-type periodic orbits; Collinear equilibrium; Three-body problem; Aerospace Engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Suryawanshi, J. S. (2019). Periodic Orbit Analytic Construction In The Circular Restricted Three-Body Problem. (Thesis). Old Dominion University. Retrieved from 9781687972897 ; https://digitalcommons.odu.edu/mae_etds/300

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):

Suryawanshi, Jay Shriram. “Periodic Orbit Analytic Construction In The Circular Restricted Three-Body Problem.” 2019. Thesis, Old Dominion University. Accessed October 30, 2020. 9781687972897 ; https://digitalcommons.odu.edu/mae_etds/300.

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

MLA Handbook (7th Edition):

Suryawanshi, Jay Shriram. “Periodic Orbit Analytic Construction In The Circular Restricted Three-Body Problem.” 2019. Web. 30 Oct 2020.

Vancouver:

Suryawanshi JS. Periodic Orbit Analytic Construction In The Circular Restricted Three-Body Problem. [Internet] [Thesis]. Old Dominion University; 2019. [cited 2020 Oct 30]. Available from: 9781687972897 ; https://digitalcommons.odu.edu/mae_etds/300.

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

Council of Science Editors:

Suryawanshi JS. Periodic Orbit Analytic Construction In The Circular Restricted Three-Body Problem. [Thesis]. Old Dominion University; 2019. Available from: 9781687972897 ; https://digitalcommons.odu.edu/mae_etds/300

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


University of Texas – Austin

15. -9471-2196. Exploration and optimization of low-energy capture options at Jovian moons.

Degree: PhD, Aerospace Engineering, 2018, University of Texas – Austin

 A key trade-off for planetary system exploration is the fuel cost required versus science data obtained. Historically, planetary systems have been explored utilizing multiple flybys,… (more)

Subjects/Keywords: Low-energy dynamics; Periodic orbits; Capture; Europa; Primer vector; Three-body problem

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

-9471-2196. (2018). Exploration and optimization of low-energy capture options at Jovian moons. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/68928

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Chicago Manual of Style (16th Edition):

-9471-2196. “Exploration and optimization of low-energy capture options at Jovian moons.” 2018. Doctoral Dissertation, University of Texas – Austin. Accessed October 30, 2020. http://hdl.handle.net/2152/68928.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

MLA Handbook (7th Edition):

-9471-2196. “Exploration and optimization of low-energy capture options at Jovian moons.” 2018. Web. 30 Oct 2020.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Vancouver:

-9471-2196. Exploration and optimization of low-energy capture options at Jovian moons. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2018. [cited 2020 Oct 30]. Available from: http://hdl.handle.net/2152/68928.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Council of Science Editors:

-9471-2196. Exploration and optimization of low-energy capture options at Jovian moons. [Doctoral Dissertation]. University of Texas – Austin; 2018. Available from: http://hdl.handle.net/2152/68928

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete


Luleå University of Technology

16. Celik, Onur. ORBITAL ENVIRONMENT CONSIDERATIONS DURING THE CLOSE APPROACH PHASE OF MISSIONS TO SMALL BODIES.

Degree: 2016, Luleå University of Technology

Missions to small bodies have become increasingly attractive in recent years, firstly, due to their scientific value, but also because of their potential risk… (more)

Subjects/Keywords: Technology; Small body exploration; Binary asteroids; Ballistic landing; Natural trajectories; CubeSat; The Circular Restricted Three Body Problem; Teknik

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Celik, O. (2016). ORBITAL ENVIRONMENT CONSIDERATIONS DURING THE CLOSE APPROACH PHASE OF MISSIONS TO SMALL BODIES. (Thesis). Luleå University of Technology. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-47143

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):

Celik, Onur. “ORBITAL ENVIRONMENT CONSIDERATIONS DURING THE CLOSE APPROACH PHASE OF MISSIONS TO SMALL BODIES.” 2016. Thesis, Luleå University of Technology. Accessed October 30, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-47143.

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

MLA Handbook (7th Edition):

Celik, Onur. “ORBITAL ENVIRONMENT CONSIDERATIONS DURING THE CLOSE APPROACH PHASE OF MISSIONS TO SMALL BODIES.” 2016. Web. 30 Oct 2020.

Vancouver:

Celik O. ORBITAL ENVIRONMENT CONSIDERATIONS DURING THE CLOSE APPROACH PHASE OF MISSIONS TO SMALL BODIES. [Internet] [Thesis]. Luleå University of Technology; 2016. [cited 2020 Oct 30]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-47143.

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

Council of Science Editors:

Celik O. ORBITAL ENVIRONMENT CONSIDERATIONS DURING THE CLOSE APPROACH PHASE OF MISSIONS TO SMALL BODIES. [Thesis]. Luleå University of Technology; 2016. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-47143

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


Purdue University

17. Guzzetti, Davide. Coupled orbit-attitude mission design in the circular restricted three-body problem.

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

  Trajectory design increasingly leverages multi-body dynamical structures that are based on an understanding of various types of orbits in the Circular Restricted Three-Body Problem(more)

Subjects/Keywords: Applied sciences; Libration points; Multi-body systems; Periodic solutions; Solar sails; Spacecraft attitude; Three-body problem; Aerospace Engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Guzzetti, D. (2016). Coupled orbit-attitude mission design in the circular restricted three-body problem. (Doctoral Dissertation). Purdue University. Retrieved from https://docs.lib.purdue.edu/open_access_dissertations/657

Chicago Manual of Style (16th Edition):

Guzzetti, Davide. “Coupled orbit-attitude mission design in the circular restricted three-body problem.” 2016. Doctoral Dissertation, Purdue University. Accessed October 30, 2020. https://docs.lib.purdue.edu/open_access_dissertations/657.

MLA Handbook (7th Edition):

Guzzetti, Davide. “Coupled orbit-attitude mission design in the circular restricted three-body problem.” 2016. Web. 30 Oct 2020.

Vancouver:

Guzzetti D. Coupled orbit-attitude mission design in the circular restricted three-body problem. [Internet] [Doctoral dissertation]. Purdue University; 2016. [cited 2020 Oct 30]. Available from: https://docs.lib.purdue.edu/open_access_dissertations/657.

Council of Science Editors:

Guzzetti D. Coupled orbit-attitude mission design in the circular restricted three-body problem. [Doctoral Dissertation]. Purdue University; 2016. Available from: https://docs.lib.purdue.edu/open_access_dissertations/657

18. Alexandre Lacerda Machuy Francisco. Estudo de trajetórias para veículos espacais utilizando captura gravitacional.

Degree: 2009, Instituto Nacional de Pesquisas Espaciais

Vindo de fora da esfera de influência gravitacional de um corpo celeste, um veículo espacial pode ter sua velocidade relativa a esse corpo reduzida ao… (more)

Subjects/Keywords: mecânica celeste; captura gravitacional; problema de três corpos; problema de quatro corpos; celestial mechanic; gravitacional capture; three body problem; four body problem

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Francisco, A. L. M. (2009). Estudo de trajetórias para veículos espacais utilizando captura gravitacional. (Thesis). Instituto Nacional de Pesquisas Espaciais. Retrieved from http://urlib.net/sid.inpe.br/[email protected]/2009/07.30.14.13

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):

Francisco, Alexandre Lacerda Machuy. “Estudo de trajetórias para veículos espacais utilizando captura gravitacional.” 2009. Thesis, Instituto Nacional de Pesquisas Espaciais. Accessed October 30, 2020. http://urlib.net/sid.inpe.br/[email protected]/2009/07.30.14.13.

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

MLA Handbook (7th Edition):

Francisco, Alexandre Lacerda Machuy. “Estudo de trajetórias para veículos espacais utilizando captura gravitacional.” 2009. Web. 30 Oct 2020.

Vancouver:

Francisco ALM. Estudo de trajetórias para veículos espacais utilizando captura gravitacional. [Internet] [Thesis]. Instituto Nacional de Pesquisas Espaciais; 2009. [cited 2020 Oct 30]. Available from: http://urlib.net/sid.inpe.br/[email protected]/2009/07.30.14.13.

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

Council of Science Editors:

Francisco ALM. Estudo de trajetórias para veículos espacais utilizando captura gravitacional. [Thesis]. Instituto Nacional de Pesquisas Espaciais; 2009. Available from: http://urlib.net/sid.inpe.br/[email protected]/2009/07.30.14.13

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

19. Κόλλιας, Νικόλαος. Μελέτη οικογενειών περιοδικών λύσεων γύρω από τα τριγωνικά σημεία ισορροπίας στο φωτοβαρυτικό πρόβλημα των τριών σωμάτων.

Degree: 2008, University of Patras

Αντικείμενο της παρούσης διπλωματικής εργασίας αποτελεί το Φωτοβαρυτικό Πρόβλημα των Τριών Σωμάτων, ένα άλυτο πρόβλημα που απασχόλησε και εξακολουθεί να απασχολεί τον τομέα των Εφαρμοσμένων… (more)

Subjects/Keywords: Φωτοβαρυτικό πρόβλημα των τριών σωμάτων; Τριγωνικά σημεία ισορροπίας; 521; Photogravitational three body problem; Triangular equilibrium points

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Κόλλιας, . (2008). Μελέτη οικογενειών περιοδικών λύσεων γύρω από τα τριγωνικά σημεία ισορροπίας στο φωτοβαρυτικό πρόβλημα των τριών σωμάτων. (Masters Thesis). University of Patras. Retrieved from http://nemertes.lis.upatras.gr/jspui/handle/10889/1074

Chicago Manual of Style (16th Edition):

Κόλλιας, Νικόλαος. “Μελέτη οικογενειών περιοδικών λύσεων γύρω από τα τριγωνικά σημεία ισορροπίας στο φωτοβαρυτικό πρόβλημα των τριών σωμάτων.” 2008. Masters Thesis, University of Patras. Accessed October 30, 2020. http://nemertes.lis.upatras.gr/jspui/handle/10889/1074.

MLA Handbook (7th Edition):

Κόλλιας, Νικόλαος. “Μελέτη οικογενειών περιοδικών λύσεων γύρω από τα τριγωνικά σημεία ισορροπίας στο φωτοβαρυτικό πρόβλημα των τριών σωμάτων.” 2008. Web. 30 Oct 2020.

Vancouver:

Κόλλιας . Μελέτη οικογενειών περιοδικών λύσεων γύρω από τα τριγωνικά σημεία ισορροπίας στο φωτοβαρυτικό πρόβλημα των τριών σωμάτων. [Internet] [Masters thesis]. University of Patras; 2008. [cited 2020 Oct 30]. Available from: http://nemertes.lis.upatras.gr/jspui/handle/10889/1074.

Council of Science Editors:

Κόλλιας . Μελέτη οικογενειών περιοδικών λύσεων γύρω από τα τριγωνικά σημεία ισορροπίας στο φωτοβαρυτικό πρόβλημα των τριών σωμάτων. [Masters Thesis]. University of Patras; 2008. Available from: http://nemertes.lis.upatras.gr/jspui/handle/10889/1074


Penn State University

20. Scott, Christopher James. Transfer and Capture into Distant Retrograde Orbits .

Degree: 2010, Penn State University

 This dissertation utilizes theory and techniques derived from the fields of dynamical systems theory, astrodyanamics, celestial mechanics, and fluid mechanics to analyze the phenomenon of… (more)

Subjects/Keywords: circular restricted three body problem; Astrodynamics; CR3BP; satellite capture

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Scott, C. J. (2010). Transfer and Capture into Distant Retrograde Orbits . (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/10471

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):

Scott, Christopher James. “Transfer and Capture into Distant Retrograde Orbits .” 2010. Thesis, Penn State University. Accessed October 30, 2020. https://submit-etda.libraries.psu.edu/catalog/10471.

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

MLA Handbook (7th Edition):

Scott, Christopher James. “Transfer and Capture into Distant Retrograde Orbits .” 2010. Web. 30 Oct 2020.

Vancouver:

Scott CJ. Transfer and Capture into Distant Retrograde Orbits . [Internet] [Thesis]. Penn State University; 2010. [cited 2020 Oct 30]. Available from: https://submit-etda.libraries.psu.edu/catalog/10471.

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

Council of Science Editors:

Scott CJ. Transfer and Capture into Distant Retrograde Orbits . [Thesis]. Penn State University; 2010. Available from: https://submit-etda.libraries.psu.edu/catalog/10471

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


Penn State University

21. Nayyar, Mollik. Optimal Earth Return Transfers from Lagrange Point Orbits Using Particle Swarm Optimization.

Degree: 2016, Penn State University

 A future where space mining and cargo transportation is fast approaching reality, for such a future, one needs a way to efficiently transport the materials… (more)

Subjects/Keywords: Three body system; Lagrange points; manifolds; optimization; particle swarm; PSO; Dynamical Systems; Optimal Transfers; Astrodynamics; Lagrange Point Orbits; LPO; Lambert's Problem

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Nayyar, M. (2016). Optimal Earth Return Transfers from Lagrange Point Orbits Using Particle Swarm Optimization. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/12617mxn244

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):

Nayyar, Mollik. “Optimal Earth Return Transfers from Lagrange Point Orbits Using Particle Swarm Optimization.” 2016. Thesis, Penn State University. Accessed October 30, 2020. https://submit-etda.libraries.psu.edu/catalog/12617mxn244.

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

MLA Handbook (7th Edition):

Nayyar, Mollik. “Optimal Earth Return Transfers from Lagrange Point Orbits Using Particle Swarm Optimization.” 2016. Web. 30 Oct 2020.

Vancouver:

Nayyar M. Optimal Earth Return Transfers from Lagrange Point Orbits Using Particle Swarm Optimization. [Internet] [Thesis]. Penn State University; 2016. [cited 2020 Oct 30]. Available from: https://submit-etda.libraries.psu.edu/catalog/12617mxn244.

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

Council of Science Editors:

Nayyar M. Optimal Earth Return Transfers from Lagrange Point Orbits Using Particle Swarm Optimization. [Thesis]. Penn State University; 2016. Available from: https://submit-etda.libraries.psu.edu/catalog/12617mxn244

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

22. Ζαγούρας, Χαράλαμπος Γ. Δευτέρας και τρίτης τάξεως μεταβολαί εις το περιορισμένον πρόβλημα των τριών σωμάτων.

Degree: 1973, University of Patras

Subjects/Keywords: Πρόβλημα των τριών σωμάτων; 515.352; Three body problem

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Ζαγούρας, . . (1973). Δευτέρας και τρίτης τάξεως μεταβολαί εις το περιορισμένον πρόβλημα των τριών σωμάτων. (Doctoral Dissertation). University of Patras. Retrieved from http://nemertes.lis.upatras.gr/jspui/handle/10889/3578

Chicago Manual of Style (16th Edition):

Ζαγούρας, Χαράλαμπος Γ. “Δευτέρας και τρίτης τάξεως μεταβολαί εις το περιορισμένον πρόβλημα των τριών σωμάτων.” 1973. Doctoral Dissertation, University of Patras. Accessed October 30, 2020. http://nemertes.lis.upatras.gr/jspui/handle/10889/3578.

MLA Handbook (7th Edition):

Ζαγούρας, Χαράλαμπος Γ. “Δευτέρας και τρίτης τάξεως μεταβολαί εις το περιορισμένον πρόβλημα των τριών σωμάτων.” 1973. Web. 30 Oct 2020.

Vancouver:

Ζαγούρας . Δευτέρας και τρίτης τάξεως μεταβολαί εις το περιορισμένον πρόβλημα των τριών σωμάτων. [Internet] [Doctoral dissertation]. University of Patras; 1973. [cited 2020 Oct 30]. Available from: http://nemertes.lis.upatras.gr/jspui/handle/10889/3578.

Council of Science Editors:

Ζαγούρας . Δευτέρας και τρίτης τάξεως μεταβολαί εις το περιορισμένον πρόβλημα των τριών σωμάτων. [Doctoral Dissertation]. University of Patras; 1973. Available from: http://nemertes.lis.upatras.gr/jspui/handle/10889/3578

23. Παπαϊώννου, Απόστολος Ι. Επτά νέαι οικογένειαι τριδιάστατων περιοδικών λύσεων διπλής συμμετρίας του περιωρισμένου προβλήματος των τριών σωμάτων.

Degree: 1974, University of Patras

Subjects/Keywords: Πρόβλημα των τριών σωμάτων; 515.352; Three body problem

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Παπαϊώννου, . . (1974). Επτά νέαι οικογένειαι τριδιάστατων περιοδικών λύσεων διπλής συμμετρίας του περιωρισμένου προβλήματος των τριών σωμάτων. (Doctoral Dissertation). University of Patras. Retrieved from http://nemertes.lis.upatras.gr/jspui/handle/10889/3801

Chicago Manual of Style (16th Edition):

Παπαϊώννου, Απόστολος Ι. “Επτά νέαι οικογένειαι τριδιάστατων περιοδικών λύσεων διπλής συμμετρίας του περιωρισμένου προβλήματος των τριών σωμάτων.” 1974. Doctoral Dissertation, University of Patras. Accessed October 30, 2020. http://nemertes.lis.upatras.gr/jspui/handle/10889/3801.

MLA Handbook (7th Edition):

Παπαϊώννου, Απόστολος Ι. “Επτά νέαι οικογένειαι τριδιάστατων περιοδικών λύσεων διπλής συμμετρίας του περιωρισμένου προβλήματος των τριών σωμάτων.” 1974. Web. 30 Oct 2020.

Vancouver:

Παπαϊώννου . Επτά νέαι οικογένειαι τριδιάστατων περιοδικών λύσεων διπλής συμμετρίας του περιωρισμένου προβλήματος των τριών σωμάτων. [Internet] [Doctoral dissertation]. University of Patras; 1974. [cited 2020 Oct 30]. Available from: http://nemertes.lis.upatras.gr/jspui/handle/10889/3801.

Council of Science Editors:

Παπαϊώννου . Επτά νέαι οικογένειαι τριδιάστατων περιοδικών λύσεων διπλής συμμετρίας του περιωρισμένου προβλήματος των τριών σωμάτων. [Doctoral Dissertation]. University of Patras; 1974. Available from: http://nemertes.lis.upatras.gr/jspui/handle/10889/3801


University of Surrey

24. Gonul, Bulent. Extended adiabatic treatments of continuum channels in nuclear stripping pickup reactions.

Degree: PhD, 1994, University of Surrey

 Although the quasi-adiabatic calculations have led to an improved description of the measured observables, the theoretical justifications of the assumptions made in the model have… (more)

Subjects/Keywords: 530.1; Quasi-adiabatic theory; Three-body problem

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Gonul, B. (1994). Extended adiabatic treatments of continuum channels in nuclear stripping pickup reactions. (Doctoral Dissertation). University of Surrey. Retrieved from http://epubs.surrey.ac.uk/844378/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.308410

Chicago Manual of Style (16th Edition):

Gonul, Bulent. “Extended adiabatic treatments of continuum channels in nuclear stripping pickup reactions.” 1994. Doctoral Dissertation, University of Surrey. Accessed October 30, 2020. http://epubs.surrey.ac.uk/844378/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.308410.

MLA Handbook (7th Edition):

Gonul, Bulent. “Extended adiabatic treatments of continuum channels in nuclear stripping pickup reactions.” 1994. Web. 30 Oct 2020.

Vancouver:

Gonul B. Extended adiabatic treatments of continuum channels in nuclear stripping pickup reactions. [Internet] [Doctoral dissertation]. University of Surrey; 1994. [cited 2020 Oct 30]. Available from: http://epubs.surrey.ac.uk/844378/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.308410.

Council of Science Editors:

Gonul B. Extended adiabatic treatments of continuum channels in nuclear stripping pickup reactions. [Doctoral Dissertation]. University of Surrey; 1994. Available from: http://epubs.surrey.ac.uk/844378/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.308410


Hong Kong University of Science and Technology

25. Chi, Xuguang. A non-variational approach to the quantum three-body coulomb problem.

Degree: 2004, Hong Kong University of Science and Technology

 This thesis presents a general non-variational approach to the solution of three-body Schrödinger's equation with Coulomb interactions, based on the utilization of symmetries intrinsic to… (more)

Subjects/Keywords: Coulomb functions ; Quantum theory ; Mathematical physics ; Three-body problem

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Chi, X. (2004). A non-variational approach to the quantum three-body coulomb problem. (Thesis). Hong Kong University of Science and Technology. Retrieved from http://repository.ust.hk/ir/Record/1783.1-2356 ; https://doi.org/10.14711/thesis-b849116 ; http://repository.ust.hk/ir/bitstream/1783.1-2356/1/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):

Chi, Xuguang. “A non-variational approach to the quantum three-body coulomb problem.” 2004. Thesis, Hong Kong University of Science and Technology. Accessed October 30, 2020. http://repository.ust.hk/ir/Record/1783.1-2356 ; https://doi.org/10.14711/thesis-b849116 ; http://repository.ust.hk/ir/bitstream/1783.1-2356/1/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):

Chi, Xuguang. “A non-variational approach to the quantum three-body coulomb problem.” 2004. Web. 30 Oct 2020.

Vancouver:

Chi X. A non-variational approach to the quantum three-body coulomb problem. [Internet] [Thesis]. Hong Kong University of Science and Technology; 2004. [cited 2020 Oct 30]. Available from: http://repository.ust.hk/ir/Record/1783.1-2356 ; https://doi.org/10.14711/thesis-b849116 ; http://repository.ust.hk/ir/bitstream/1783.1-2356/1/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:

Chi X. A non-variational approach to the quantum three-body coulomb problem. [Thesis]. Hong Kong University of Science and Technology; 2004. Available from: http://repository.ust.hk/ir/Record/1783.1-2356 ; https://doi.org/10.14711/thesis-b849116 ; http://repository.ust.hk/ir/bitstream/1783.1-2356/1/th_redirect.html

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


Delft University of Technology

26. de Boer, Roderick (author). Time-Optimal Transfers Between Planar Solar-Sail Libration Point Orbits.

Degree: 2020, Delft University of Technology

This paper presents time-optimal transfer trajectories between planar solar-sail displaced libration point orbits around the L1 and L2 points of the Sun-Earth and Earth-Moon systems.… (more)

Subjects/Keywords: Solar sailing; Circular restricted three-body problem; Libration point orbit; Optimal Control; Astrodynamics; Transfer orbits; Trajectory optimisation; Multiple shooting; Collocation

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

de Boer, R. (. (2020). Time-Optimal Transfers Between Planar Solar-Sail Libration Point Orbits. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:c97e4c70-cf7a-4f7d-aed2-e2782b141e14

Chicago Manual of Style (16th Edition):

de Boer, Roderick (author). “Time-Optimal Transfers Between Planar Solar-Sail Libration Point Orbits.” 2020. Masters Thesis, Delft University of Technology. Accessed October 30, 2020. http://resolver.tudelft.nl/uuid:c97e4c70-cf7a-4f7d-aed2-e2782b141e14.

MLA Handbook (7th Edition):

de Boer, Roderick (author). “Time-Optimal Transfers Between Planar Solar-Sail Libration Point Orbits.” 2020. Web. 30 Oct 2020.

Vancouver:

de Boer R(. Time-Optimal Transfers Between Planar Solar-Sail Libration Point Orbits. [Internet] [Masters thesis]. Delft University of Technology; 2020. [cited 2020 Oct 30]. Available from: http://resolver.tudelft.nl/uuid:c97e4c70-cf7a-4f7d-aed2-e2782b141e14.

Council of Science Editors:

de Boer R(. Time-Optimal Transfers Between Planar Solar-Sail Libration Point Orbits. [Masters Thesis]. Delft University of Technology; 2020. Available from: http://resolver.tudelft.nl/uuid:c97e4c70-cf7a-4f7d-aed2-e2782b141e14

27. Pousse, Alexandre. Le quasi-satellites et autres configurations remarquables en résonance co-orbitale : Around quasi-satellites and remarkable configurations in the co-orbital resonance.

Degree: Docteur es, Mécanique céleste, 2016, Paris Sciences et Lettres (ComUE)

L'ensemble des travaux menés au cours de cette thèse concerne l'étude de la résonance co-orbitale. Ce domaine de trajectoires particulières, où un astéroïde et une… (more)

Subjects/Keywords: Mécanique céleste; Résonance co-Orbitale; Problème à trois corps; Celestial mechanics; Co-Orbital resonance; Three-Body problem; 520

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Pousse, A. (2016). Le quasi-satellites et autres configurations remarquables en résonance co-orbitale : Around quasi-satellites and remarkable configurations in the co-orbital resonance. (Doctoral Dissertation). Paris Sciences et Lettres (ComUE). Retrieved from http://www.theses.fr/2016PSLEO006

Chicago Manual of Style (16th Edition):

Pousse, Alexandre. “Le quasi-satellites et autres configurations remarquables en résonance co-orbitale : Around quasi-satellites and remarkable configurations in the co-orbital resonance.” 2016. Doctoral Dissertation, Paris Sciences et Lettres (ComUE). Accessed October 30, 2020. http://www.theses.fr/2016PSLEO006.

MLA Handbook (7th Edition):

Pousse, Alexandre. “Le quasi-satellites et autres configurations remarquables en résonance co-orbitale : Around quasi-satellites and remarkable configurations in the co-orbital resonance.” 2016. Web. 30 Oct 2020.

Vancouver:

Pousse A. Le quasi-satellites et autres configurations remarquables en résonance co-orbitale : Around quasi-satellites and remarkable configurations in the co-orbital resonance. [Internet] [Doctoral dissertation]. Paris Sciences et Lettres (ComUE); 2016. [cited 2020 Oct 30]. Available from: http://www.theses.fr/2016PSLEO006.

Council of Science Editors:

Pousse A. Le quasi-satellites et autres configurations remarquables en résonance co-orbitale : Around quasi-satellites and remarkable configurations in the co-orbital resonance. [Doctoral Dissertation]. Paris Sciences et Lettres (ComUE); 2016. Available from: http://www.theses.fr/2016PSLEO006


Aristotle University Of Thessaloniki (AUTH); Αριστοτέλειο Πανεπιστήμιο Θεσσαλονίκης (ΑΠΘ)

28. Antoniadou, Kyriaki. Dynamics of planetary systems in resonances: from the planar to the spatial case.

Degree: 2014, Aristotle University Of Thessaloniki (AUTH); Αριστοτέλειο Πανεπιστήμιο Θεσσαλονίκης (ΑΠΘ)

 Over the last decades, there has been a tremendous increase of extrasolar planetary systems discoveries. Many of such systems consist of more than one planet… (more)

Subjects/Keywords: Εξωπλανητικά συστήματα; Πρόβλημα τριών σωμάτων; Συντονισμένη κίνηση; Πλανητική μετανάστευση; Exoplanetary systems; Three body problem; Resonant motion; Planetary migration

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Antoniadou, K. (2014). Dynamics of planetary systems in resonances: from the planar to the spatial case. (Thesis). Aristotle University Of Thessaloniki (AUTH); Αριστοτέλειο Πανεπιστήμιο Θεσσαλονίκης (ΑΠΘ). Retrieved from http://hdl.handle.net/10442/hedi/34917

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):

Antoniadou, Kyriaki. “Dynamics of planetary systems in resonances: from the planar to the spatial case.” 2014. Thesis, Aristotle University Of Thessaloniki (AUTH); Αριστοτέλειο Πανεπιστήμιο Θεσσαλονίκης (ΑΠΘ). Accessed October 30, 2020. http://hdl.handle.net/10442/hedi/34917.

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

MLA Handbook (7th Edition):

Antoniadou, Kyriaki. “Dynamics of planetary systems in resonances: from the planar to the spatial case.” 2014. Web. 30 Oct 2020.

Vancouver:

Antoniadou K. Dynamics of planetary systems in resonances: from the planar to the spatial case. [Internet] [Thesis]. Aristotle University Of Thessaloniki (AUTH); Αριστοτέλειο Πανεπιστήμιο Θεσσαλονίκης (ΑΠΘ); 2014. [cited 2020 Oct 30]. Available from: http://hdl.handle.net/10442/hedi/34917.

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

Council of Science Editors:

Antoniadou K. Dynamics of planetary systems in resonances: from the planar to the spatial case. [Thesis]. Aristotle University Of Thessaloniki (AUTH); Αριστοτέλειο Πανεπιστήμιο Θεσσαλονίκης (ΑΠΘ); 2014. Available from: http://hdl.handle.net/10442/hedi/34917

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


University of Texas – Austin

29. -9883-5836. Patched periodic orbits : a systematic strategy for low-energy trajectory and moon tour design.

Degree: PhD, Aerospace Engineering, 2018, University of Texas – Austin

 The implementation of low-energy trajectories has opened a new paradigm in trajectory design, where, at the cost of long transfer times, low-fuel consumption missions opened… (more)

Subjects/Keywords: Low-energy trajectory; Astrodynamics; Celestial mechanics; Circular restricted three-body problem; Periodic orbits; Mission design; Trajectory optimization; Galilean moon tours

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

-9883-5836. (2018). Patched periodic orbits : a systematic strategy for low-energy trajectory and moon tour design. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/68679

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Chicago Manual of Style (16th Edition):

-9883-5836. “Patched periodic orbits : a systematic strategy for low-energy trajectory and moon tour design.” 2018. Doctoral Dissertation, University of Texas – Austin. Accessed October 30, 2020. http://hdl.handle.net/2152/68679.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

MLA Handbook (7th Edition):

-9883-5836. “Patched periodic orbits : a systematic strategy for low-energy trajectory and moon tour design.” 2018. Web. 30 Oct 2020.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Vancouver:

-9883-5836. Patched periodic orbits : a systematic strategy for low-energy trajectory and moon tour design. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2018. [cited 2020 Oct 30]. Available from: http://hdl.handle.net/2152/68679.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Council of Science Editors:

-9883-5836. Patched periodic orbits : a systematic strategy for low-energy trajectory and moon tour design. [Doctoral Dissertation]. University of Texas – Austin; 2018. Available from: http://hdl.handle.net/2152/68679

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete


Queens University

30. Mansur, Abdalla. Instability of Periodic Orbits of Some Rhombus and Parallelogram Four Body Problems .

Degree: Mathematics and Statistics, 2012, Queens University

 The rhombus and parallelogram orbits are interesting families of periodic solutions, which come from celestial mechanics and the N-body problem. Variational methods with finite order… (more)

Subjects/Keywords: N-Body Problem

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Mansur, A. (2012). Instability of Periodic Orbits of Some Rhombus and Parallelogram Four Body Problems . (Thesis). Queens University. Retrieved from http://hdl.handle.net/1974/7650

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):

Mansur, Abdalla. “Instability of Periodic Orbits of Some Rhombus and Parallelogram Four Body Problems .” 2012. Thesis, Queens University. Accessed October 30, 2020. http://hdl.handle.net/1974/7650.

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

MLA Handbook (7th Edition):

Mansur, Abdalla. “Instability of Periodic Orbits of Some Rhombus and Parallelogram Four Body Problems .” 2012. Web. 30 Oct 2020.

Vancouver:

Mansur A. Instability of Periodic Orbits of Some Rhombus and Parallelogram Four Body Problems . [Internet] [Thesis]. Queens University; 2012. [cited 2020 Oct 30]. Available from: http://hdl.handle.net/1974/7650.

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

Council of Science Editors:

Mansur A. Instability of Periodic Orbits of Some Rhombus and Parallelogram Four Body Problems . [Thesis]. Queens University; 2012. Available from: http://hdl.handle.net/1974/7650

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

[1] [2] [3] [4] [5] … [847]

.