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You searched for subject:(Two body problem). Showing records 1 – 12 of 12 total matches.

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University of Johannesburg

1. 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

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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 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 (7th 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

Note: this citation may be lacking information needed for this citation format:
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

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 (6th 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

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):

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.

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

MLA Handbook (7th 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.

Note: this citation may be lacking information needed for this citation format:
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

Note: this citation may be lacking information needed for this citation format:
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

 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 (6th 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

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):

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.

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

MLA Handbook (7th 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.

Note: this citation may be lacking information needed for this citation format:
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

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


Brno University of Technology

4. Bahník, Michal. Základy pohybu vesmírných těles .

Degree: 2013, Brno University of Technology

 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 (6th Edition):

Bahník, M. (2013). Základy pohybu vesmírných těles . (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 .” 2013. Thesis, Brno University of Technology. Accessed August 18, 2019. 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 .” 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.

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 . [Thesis]. Brno University of Technology; 2013. 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


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

 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 (6th 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

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):

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.

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

MLA Handbook (7th 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.

Note: this citation may be lacking information needed for this citation format:
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

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

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

Degree: Mathematics, 2013, Linnaeus University

  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… 

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APA (6th 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

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):

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.

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

MLA Handbook (7th 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.

Note: this citation may be lacking information needed for this citation format:
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

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


MIT

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

Degree: 1975, MIT

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

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APA (6th Edition):

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

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):

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

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

MLA Handbook (7th 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.

Note: this citation may be lacking information needed for this citation format:
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

Note: this citation may be lacking information needed for this citation format:
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

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

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APA (6th 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

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):

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.

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

MLA Handbook (7th 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.

Note: this citation may be lacking information needed for this citation format:
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

Note: this citation may be lacking information needed for this citation format:
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

 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 (6th 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 (16th 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 (7th 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

  The two body problem and the rocket equation <b>r̈</b> + ∊ α <b>ṙ</b> + k/r3<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

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APA (6th 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 (16th 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 (7th 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

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

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APA (6th 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

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):

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.

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

MLA Handbook (7th 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.

Note: this citation may be lacking information needed for this citation format:
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

Note: this citation may be lacking information needed for this citation format:
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

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

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APA (6th 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 (16th 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 (7th 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/ ;

.