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University of Johannesburg

1. Anderson, Keegan Doig. Gravitational capture.

Degree: 2012, University of Johannesburg

URL: http://hdl.handle.net/10210/8053

►

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

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

APA (6^{th} 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 (16^{th} Edition):

Anderson, Keegan Doig. “Gravitational capture.” 2012. Thesis, University of Johannesburg. Accessed August 18, 2019. 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 (7^{th} Edition):

Anderson, Keegan Doig. “Gravitational capture.” 2012. Web. 18 Aug 2019.

Vancouver:

Anderson KD. Gravitational capture. [Internet] [Thesis]. University of Johannesburg; 2012. [cited 2019 Aug 18]. 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

Not specified: Masters Thesis or Doctoral Dissertation

University of British Columbia

2.
Barkham, Peter George Douglas.
Some aspects of three and four-*body* dynamics
.

Degree: 1974, University of British Columbia

URL: http://hdl.handle.net/2429/18937

► *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

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

APA (6^{th} Edition):

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

Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^{th} Edition):

Barkham, Peter George Douglas. “Some aspects of three and four-body dynamics .” 1974. Thesis, University of British Columbia. Accessed August 18, 2019. http://hdl.handle.net/2429/18937.

Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^{th} Edition):

Barkham, Peter George Douglas. “Some aspects of three and four-body dynamics .” 1974. Web. 18 Aug 2019.

Vancouver:

Barkham PGD. Some aspects of three and four-body dynamics . [Internet] [Thesis]. University of British Columbia; 1974. [cited 2019 Aug 18]. Available from: http://hdl.handle.net/2429/18937.

Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

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

Not specified: Masters Thesis or Doctoral Dissertation

University of Texas – Austin

3.
Ottesen, David Ryan.
The dynamics of deployment and observation of a rigid *body* spacecraft system in the linear and non-linear *two*-*body* * problem*.

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

URL: http://hdl.handle.net/2152/19685

► Modern space situational awareness entails the detection, tracking, identification, and characterization of resident space objects. Characterization is typically accomplished through the use of ground and…
(more)

Subjects/Keywords: Modern space situational awareness; Two-body problem; Deployment; Observation; Floquet controller; Rigid body dynamics

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APA (6^{th} Edition):

Ottesen, D. R. (2012). The dynamics of deployment and observation of a rigid body spacecraft system in the linear and non-linear two-body problem. (Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/19685

Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^{th} Edition):

Ottesen, David Ryan. “The dynamics of deployment and observation of a rigid body spacecraft system in the linear and non-linear two-body problem.” 2012. Thesis, University of Texas – Austin. Accessed August 18, 2019. http://hdl.handle.net/2152/19685.

Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^{th} Edition):

Ottesen, David Ryan. “The dynamics of deployment and observation of a rigid body spacecraft system in the linear and non-linear two-body problem.” 2012. Web. 18 Aug 2019.

Vancouver:

Ottesen DR. The dynamics of deployment and observation of a rigid body spacecraft system in the linear and non-linear two-body problem. [Internet] [Thesis]. University of Texas – Austin; 2012. [cited 2019 Aug 18]. Available from: http://hdl.handle.net/2152/19685.

Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Ottesen DR. The dynamics of deployment and observation of a rigid body spacecraft system in the linear and non-linear two-body problem. [Thesis]. University of Texas – Austin; 2012. Available from: http://hdl.handle.net/2152/19685

Not specified: Masters Thesis or Doctoral Dissertation

Brno University of Technology

4. Bahník, Michal. Základy pohybu vesmírných těles .

Degree: 2013, Brno University of Technology

URL: http://hdl.handle.net/11012/26440

► Tato bakalářská práce je přehledovým textem, který se zabývá problematikou pohybu vesmírných těles. Je rozebírán problém jednoho, dvou a tří těles. U prvních dvou úloh…
(more)

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

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

APA (6^{th} Edition):

Bahník, M. (2013). Základy pohybu vesmírných těles . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/26440

Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^{th} Edition):

Bahník, Michal. “Základy pohybu vesmírných těles .” 2013. Thesis, Brno University of Technology. Accessed August 18, 2019. http://hdl.handle.net/11012/26440.

Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^{th} Edition):

Bahník, Michal. “Základy pohybu vesmírných těles .” 2013. Web. 18 Aug 2019.

Vancouver:

Bahník M. Základy pohybu vesmírných těles . [Internet] [Thesis]. Brno University of Technology; 2013. [cited 2019 Aug 18]. Available from: http://hdl.handle.net/11012/26440.

Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Bahník M. Základy pohybu vesmírných těles . [Thesis]. Brno University of Technology; 2013. Available from: http://hdl.handle.net/11012/26440

Not specified: Masters Thesis or Doctoral Dissertation

University of Missouri – Columbia

5.
Heitzman, Michael Thomas.
A free boundary gas dynamic model as a *two*-*body* field theory * problem*.

Degree: 2009, University of Missouri – Columbia

URL: https://doi.org/10.32469/10355/7017

► Motivated by the *two*-*body* *problem* in the classical field theories of electrodynamics and gravitation, in which finite propagation speeds lead to radiation reaction and runaway…
(more)

Subjects/Keywords: Two-body problem; Field theory (Physics); Gas dynamics – Mathematical models; Differential equations

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

APA (6^{th} Edition):

Heitzman, M. T. (2009). A free boundary gas dynamic model as a two-body field theory problem. (Thesis). University of Missouri – Columbia. Retrieved from https://doi.org/10.32469/10355/7017

Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^{th} Edition):

Heitzman, Michael Thomas. “A free boundary gas dynamic model as a two-body field theory problem.” 2009. Thesis, University of Missouri – Columbia. Accessed August 18, 2019. https://doi.org/10.32469/10355/7017.

Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^{th} Edition):

Heitzman, Michael Thomas. “A free boundary gas dynamic model as a two-body field theory problem.” 2009. Web. 18 Aug 2019.

Vancouver:

Heitzman MT. A free boundary gas dynamic model as a two-body field theory problem. [Internet] [Thesis]. University of Missouri – Columbia; 2009. [cited 2019 Aug 18]. Available from: https://doi.org/10.32469/10355/7017.

Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Heitzman MT. A free boundary gas dynamic model as a two-body field theory problem. [Thesis]. University of Missouri – Columbia; 2009. Available from: https://doi.org/10.32469/10355/7017

Not specified: Masters Thesis or Doctoral Dissertation

6.
Gleisner, Frida.
Three solutions to the *two*-*body* * problem*.

Degree: Mathematics, 2013, Linnaeus University

URL: http://urn.kb.se/resolve?urn=urn:nbn:se:lnu:diva-26781

► The *two*-*body* *problem* consists of determining the motion of *two* gravitationally interacting bodies with given masses and initial velocities. The *problem* was first solved…
(more)

Subjects/Keywords: two-body problem; Newtonian mechanics; classical geometry; Feynman's lost lecture

…solutions to numerous
problems, the *two*-*body* *problem* is found in Proposition I, VI, XI and LVII to… …5.2
*Two* moving bodies
The solution to the *two*-*body* *problem* containing *two* bodies in motion… …*problem* differential equations are used to find the paths for
the bodies. Let M1 and M2 be *two*… …arbitrary point in space.
To simplify the *problem* we divide it into *two* parts, one part where M1… …have a solution to the first part of our
*problem*. Newton showed a *body* in orbit to describe…

Record Details Similar Records

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

APA (6^{th} Edition):

Gleisner, F. (2013). Three solutions to the two-body problem. (Thesis). Linnaeus University. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:lnu:diva-26781

Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^{th} Edition):

Gleisner, Frida. “Three solutions to the two-body problem.” 2013. Thesis, Linnaeus University. Accessed August 18, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:lnu:diva-26781.

Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^{th} Edition):

Gleisner, Frida. “Three solutions to the two-body problem.” 2013. Web. 18 Aug 2019.

Vancouver:

Gleisner F. Three solutions to the two-body problem. [Internet] [Thesis]. Linnaeus University; 2013. [cited 2019 Aug 18]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:lnu:diva-26781.

Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Gleisner F. Three solutions to the two-body problem. [Thesis]. Linnaeus University; 2013. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:lnu:diva-26781

Not specified: Masters Thesis or Doctoral Dissertation

MIT

7. Koonin, Steven E. Hydrodynamic approximations to time-dependent Hartree-Fock .

Degree: 1975, MIT

URL: http://hdl.handle.net/1721.1/98318

Subjects/Keywords: Physics; Hartree-Fock approximation; Quantum theory; Hydrodynamics; Two-body problem; Wave functions

Record Details Similar Records

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

APA (6^{th} Edition):

Koonin, S. E. (1975). Hydrodynamic approximations to time-dependent Hartree-Fock . (Thesis). MIT. Retrieved from http://hdl.handle.net/1721.1/98318

Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^{th} Edition):

Koonin, Steven E. “Hydrodynamic approximations to time-dependent Hartree-Fock .” 1975. Thesis, MIT. Accessed August 18, 2019. http://hdl.handle.net/1721.1/98318.

Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^{th} Edition):

Koonin, Steven E. “Hydrodynamic approximations to time-dependent Hartree-Fock .” 1975. Web. 18 Aug 2019.

Vancouver:

Koonin SE. Hydrodynamic approximations to time-dependent Hartree-Fock . [Internet] [Thesis]. MIT; 1975. [cited 2019 Aug 18]. Available from: http://hdl.handle.net/1721.1/98318.

Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Koonin SE. Hydrodynamic approximations to time-dependent Hartree-Fock . [Thesis]. MIT; 1975. Available from: http://hdl.handle.net/1721.1/98318

Not specified: Masters Thesis or Doctoral Dissertation

MIT

8. Fill, Thomas Joseph. Extension of Gauss' method for the solution of Kepler's equation .

Degree: 1976, MIT

URL: http://hdl.handle.net/1721.1/16383

Subjects/Keywords: Aeronautics and Astronautics; Orbits; Two-body problem; Navigation (Astronautics); Iterative methods (Mathematics)

Record Details Similar Records

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

APA (6^{th} Edition):

Fill, T. J. (1976). Extension of Gauss' method for the solution of Kepler's equation . (Thesis). MIT. Retrieved from http://hdl.handle.net/1721.1/16383

Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^{th} Edition):

Fill, Thomas Joseph. “Extension of Gauss' method for the solution of Kepler's equation .” 1976. Thesis, MIT. Accessed August 18, 2019. http://hdl.handle.net/1721.1/16383.

Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^{th} Edition):

Fill, Thomas Joseph. “Extension of Gauss' method for the solution of Kepler's equation .” 1976. Web. 18 Aug 2019.

Vancouver:

Fill TJ. Extension of Gauss' method for the solution of Kepler's equation . [Internet] [Thesis]. MIT; 1976. [cited 2019 Aug 18]. Available from: http://hdl.handle.net/1721.1/16383.

Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Fill TJ. Extension of Gauss' method for the solution of Kepler's equation . [Thesis]. MIT; 1976. Available from: http://hdl.handle.net/1721.1/16383

Not specified: Masters Thesis or Doctoral Dissertation

University of Michigan

9.
Bellerose, Julie.
The Restricted Full Three *Body* *Problem*: Applications to Binary Asteroid Exploration.

Degree: PhD, Aerospace Engineering, 2008, University of Michigan

URL: http://hdl.handle.net/2027.42/60695

► There is much current interest in understanding the formation and evolution of the small bodies of our solar system. In addition, current astronomical observations suggest…
(more)

Subjects/Keywords: Full Two Body Problem; Binary Asteroid Exploration; Restricted Full Three Body Problem; Robotic Exploration; Mission Design; Surface Dynamics and Control; Aerospace Engineering; Engineering

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

APA (6^{th} Edition):

Bellerose, J. (2008). The Restricted Full Three Body Problem: Applications to Binary Asteroid Exploration. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/60695

Chicago Manual of Style (16^{th} Edition):

Bellerose, Julie. “The Restricted Full Three Body Problem: Applications to Binary Asteroid Exploration.” 2008. Doctoral Dissertation, University of Michigan. Accessed August 18, 2019. http://hdl.handle.net/2027.42/60695.

MLA Handbook (7^{th} Edition):

Bellerose, Julie. “The Restricted Full Three Body Problem: Applications to Binary Asteroid Exploration.” 2008. Web. 18 Aug 2019.

Vancouver:

Bellerose J. The Restricted Full Three Body Problem: Applications to Binary Asteroid Exploration. [Internet] [Doctoral dissertation]. University of Michigan; 2008. [cited 2019 Aug 18]. Available from: http://hdl.handle.net/2027.42/60695.

Council of Science Editors:

Bellerose J. The Restricted Full Three Body Problem: Applications to Binary Asteroid Exploration. [Doctoral Dissertation]. University of Michigan; 2008. Available from: http://hdl.handle.net/2027.42/60695

East Tennessee State University

10.
Clark, Clayton Jeremiah.
Rocket Powered Flight as a Perturbation to the *Two*-*Body* *Problem*.

Degree: MS, Mathematical Sciences, 2005, East Tennessee State University

URL: https://dc.etsu.edu/etd/1045

► The *two* *body* *problem* and the rocket equation <b>r̈</b> + ∊ α <b>ṙ</b> + k/r^{3}<b>r</b> = <b>0</b> have been expressed in numerous ways. However,…
(more)

Subjects/Keywords: rocket flight; perturbation; two-body problem; Applied Mathematics; Non-linear Dynamics; Physical Sciences and Mathematics

Record Details Similar Records

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

APA (6^{th} Edition):

Clark, C. J. (2005). Rocket Powered Flight as a Perturbation to the Two-Body Problem. (Masters Thesis). East Tennessee State University. Retrieved from https://dc.etsu.edu/etd/1045

Chicago Manual of Style (16^{th} Edition):

Clark, Clayton Jeremiah. “Rocket Powered Flight as a Perturbation to the Two-Body Problem.” 2005. Masters Thesis, East Tennessee State University. Accessed August 18, 2019. https://dc.etsu.edu/etd/1045.

MLA Handbook (7^{th} Edition):

Clark, Clayton Jeremiah. “Rocket Powered Flight as a Perturbation to the Two-Body Problem.” 2005. Web. 18 Aug 2019.

Vancouver:

Clark CJ. Rocket Powered Flight as a Perturbation to the Two-Body Problem. [Internet] [Masters thesis]. East Tennessee State University; 2005. [cited 2019 Aug 18]. Available from: https://dc.etsu.edu/etd/1045.

Council of Science Editors:

Clark CJ. Rocket Powered Flight as a Perturbation to the Two-Body Problem. [Masters Thesis]. East Tennessee State University; 2005. Available from: https://dc.etsu.edu/etd/1045

11. Gislaine de Felipe. Manobras orbitais aplicadas aos problemas de dois e tres corpos.

Degree: 2000, Instituto Nacional de Pesquisas Espaciais

URL: http://urlib.net/sid.inpe.br/deise/2000/11.06.11.16

►

In the space activities, it is of great importance the study of the trajectories that the space vehicles should follow to complete a mission. With… (more)

Subjects/Keywords: ENGENHARIA E TECNOLOGIA ESPACIAL; MECANICA CELESTE; PROBLEMA DE DOIS CORPOS; TRANSFERENCIA ORBITAL; CELESTIAL MECHANICS; TWO BODY PROBLEM; TREE BODY PROBLEM; SPACECRAFTS ORBITS; TRAJECTORIES; PROBLEMA DE TRES CORPOS; ORBITA DE SATELITES; TRAJETORIAS; ASTRODINAMICA; ASTRODYNAMICS

Record Details Similar Records

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

APA (6^{th} Edition):

Felipe, G. d. (2000). Manobras orbitais aplicadas aos problemas de dois e tres corpos. (Thesis). Instituto Nacional de Pesquisas Espaciais. Retrieved from http://urlib.net/sid.inpe.br/deise/2000/11.06.11.16

Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^{th} Edition):

Felipe, Gislaine de. “Manobras orbitais aplicadas aos problemas de dois e tres corpos.” 2000. Thesis, Instituto Nacional de Pesquisas Espaciais. Accessed August 18, 2019. http://urlib.net/sid.inpe.br/deise/2000/11.06.11.16.

Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^{th} Edition):

Felipe, Gislaine de. “Manobras orbitais aplicadas aos problemas de dois e tres corpos.” 2000. Web. 18 Aug 2019.

Vancouver:

Felipe Gd. Manobras orbitais aplicadas aos problemas de dois e tres corpos. [Internet] [Thesis]. Instituto Nacional de Pesquisas Espaciais; 2000. [cited 2019 Aug 18]. Available from: http://urlib.net/sid.inpe.br/deise/2000/11.06.11.16.

Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Felipe Gd. Manobras orbitais aplicadas aos problemas de dois e tres corpos. [Thesis]. Instituto Nacional de Pesquisas Espaciais; 2000. Available from: http://urlib.net/sid.inpe.br/deise/2000/11.06.11.16

Not specified: Masters Thesis or Doctoral Dissertation

12. Souza, Daniel Câmara de. Eletrodinâmica variacional e o problema eletromagnético de dois corpos.

Degree: PhD, Física, 2014, University of São Paulo

URL: http://www.teses.usp.br/teses/disponiveis/43/43134/tde-26012015-213657/ ;

►

Estudamos a Eletrodinâmica de Wheeler-Feynman usando um princípio variacional para um funcional de ação finito acoplado a um problema de valor na fronteira. Para trajetórias… (more)

Subjects/Keywords: Condições de Quina de Weierstrass-Erdmann; Electromagnetic Two-Body Problem; Eletrodinâmica de Wheeler-Feynman; Equação Diferencial com Retardo Misto Dependente do Estado e do Tipo Neutro; Finite Element Methods; Método dos Elementos Finitos; Método Variacional; Problema Eletromagnético de Dois Corpos; State-Dependent Mixed-Type Neutral Differential-Delay Equations; Variational Method; Weierstrass-Erdmann Corner Conditions; Wheeler-Feynman Electrodynamics

Record Details Similar Records

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

APA (6^{th} Edition):

Souza, D. C. d. (2014). Eletrodinâmica variacional e o problema eletromagnético de dois corpos. (Doctoral Dissertation). University of São Paulo. Retrieved from http://www.teses.usp.br/teses/disponiveis/43/43134/tde-26012015-213657/ ;

Chicago Manual of Style (16^{th} Edition):

Souza, Daniel Câmara de. “Eletrodinâmica variacional e o problema eletromagnético de dois corpos.” 2014. Doctoral Dissertation, University of São Paulo. Accessed August 18, 2019. http://www.teses.usp.br/teses/disponiveis/43/43134/tde-26012015-213657/ ;.

MLA Handbook (7^{th} Edition):

Souza, Daniel Câmara de. “Eletrodinâmica variacional e o problema eletromagnético de dois corpos.” 2014. Web. 18 Aug 2019.

Vancouver:

Souza DCd. Eletrodinâmica variacional e o problema eletromagnético de dois corpos. [Internet] [Doctoral dissertation]. University of São Paulo; 2014. [cited 2019 Aug 18]. Available from: http://www.teses.usp.br/teses/disponiveis/43/43134/tde-26012015-213657/ ;.

Council of Science Editors:

Souza DCd. Eletrodinâmica variacional e o problema eletromagnético de dois corpos. [Doctoral Dissertation]. University of São Paulo; 2014. Available from: http://www.teses.usp.br/teses/disponiveis/43/43134/tde-26012015-213657/ ;