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You searched for subject:(orbit propagation). Showing records 1 – 22 of 22 total matches.

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University of Colorado

1. Jones, Brandon Allan. Efficient Models for the Evaluation and Estimation of the Gravity Field.

Degree: PhD, Aerospace Engineering Sciences, 2010, University of Colorado

  Current astrodynamics applications require a rapid evaluation of the gravity field and an efficient approach to gravity estimation. The commonly used spherical harmonic model… (more)

Subjects/Keywords: asteroid; gravity estimation; gravity modeling; orbit determination; orbit propagation; spherical harmonics; Aerospace Engineering; Astrodynamics

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APA (6th Edition):

Jones, B. A. (2010). Efficient Models for the Evaluation and Estimation of the Gravity Field. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/11

Chicago Manual of Style (16th Edition):

Jones, Brandon Allan. “Efficient Models for the Evaluation and Estimation of the Gravity Field.” 2010. Doctoral Dissertation, University of Colorado. Accessed October 31, 2020. https://scholar.colorado.edu/asen_gradetds/11.

MLA Handbook (7th Edition):

Jones, Brandon Allan. “Efficient Models for the Evaluation and Estimation of the Gravity Field.” 2010. Web. 31 Oct 2020.

Vancouver:

Jones BA. Efficient Models for the Evaluation and Estimation of the Gravity Field. [Internet] [Doctoral dissertation]. University of Colorado; 2010. [cited 2020 Oct 31]. Available from: https://scholar.colorado.edu/asen_gradetds/11.

Council of Science Editors:

Jones BA. Efficient Models for the Evaluation and Estimation of the Gravity Field. [Doctoral Dissertation]. University of Colorado; 2010. Available from: https://scholar.colorado.edu/asen_gradetds/11


Penn State University

2. Kuppa, Koundinya. Long-term Orbit Propagation Using Symplectic Integration Algorithms.

Degree: 2016, Penn State University

 Understanding the evolution of satellite orbits in the long-term is of great importance in astrodynamics. In order to achieve this, accurate propagation of the orbital… (more)

Subjects/Keywords: astrodynamics; orbital mechanics; symplectic integration; numerical integration; orbit propagation; spaceflight mechanics

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APA (6th Edition):

Kuppa, K. (2016). Long-term Orbit Propagation Using Symplectic Integration Algorithms. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/29463

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):

Kuppa, Koundinya. “Long-term Orbit Propagation Using Symplectic Integration Algorithms.” 2016. Thesis, Penn State University. Accessed October 31, 2020. https://submit-etda.libraries.psu.edu/catalog/29463.

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

MLA Handbook (7th Edition):

Kuppa, Koundinya. “Long-term Orbit Propagation Using Symplectic Integration Algorithms.” 2016. Web. 31 Oct 2020.

Vancouver:

Kuppa K. Long-term Orbit Propagation Using Symplectic Integration Algorithms. [Internet] [Thesis]. Penn State University; 2016. [cited 2020 Oct 31]. Available from: https://submit-etda.libraries.psu.edu/catalog/29463.

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

Council of Science Editors:

Kuppa K. Long-term Orbit Propagation Using Symplectic Integration Algorithms. [Thesis]. Penn State University; 2016. Available from: https://submit-etda.libraries.psu.edu/catalog/29463

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


Delft University of Technology

3. Pinardell Pons, Aleix (author). GTO debris mitigation using natural perturbations.

Degree: 2017, Delft University of Technology

 Objects ingeostationary transfer orbit (GTO) can collide with operative satellites in lowEarth orbit (LEO) and geostationary orbit (GEO). Various organisationshave laid down debris-mitigation guidelines that… (more)

Subjects/Keywords: GTO; debris; mitigation; semi-analytical propagation; Orbit modeling; perturbations

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APA (6th Edition):

Pinardell Pons, A. (. (2017). GTO debris mitigation using natural perturbations. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:f550d59a-7d15-46dd-a084-025ace46e643

Chicago Manual of Style (16th Edition):

Pinardell Pons, Aleix (author). “GTO debris mitigation using natural perturbations.” 2017. Masters Thesis, Delft University of Technology. Accessed October 31, 2020. http://resolver.tudelft.nl/uuid:f550d59a-7d15-46dd-a084-025ace46e643.

MLA Handbook (7th Edition):

Pinardell Pons, Aleix (author). “GTO debris mitigation using natural perturbations.” 2017. Web. 31 Oct 2020.

Vancouver:

Pinardell Pons A(. GTO debris mitigation using natural perturbations. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2020 Oct 31]. Available from: http://resolver.tudelft.nl/uuid:f550d59a-7d15-46dd-a084-025ace46e643.

Council of Science Editors:

Pinardell Pons A(. GTO debris mitigation using natural perturbations. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:f550d59a-7d15-46dd-a084-025ace46e643


Virginia Tech

4. Berry, Matthew M. A Variable-Step Double-Integration Multi-Step Integrator.

Degree: PhD, Aerospace and Ocean Engineering, 2004, Virginia Tech

 A new method of numerical integration is presented here, the variable-step Stormer-Cowell method. The method uses error control to regulate the step size, so larger… (more)

Subjects/Keywords: Variable-Step Integration; Orbit Propagation; Orbit Determination; Numerical Integration

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APA (6th Edition):

Berry, M. M. (2004). A Variable-Step Double-Integration Multi-Step Integrator. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/11155

Chicago Manual of Style (16th Edition):

Berry, Matthew M. “A Variable-Step Double-Integration Multi-Step Integrator.” 2004. Doctoral Dissertation, Virginia Tech. Accessed October 31, 2020. http://hdl.handle.net/10919/11155.

MLA Handbook (7th Edition):

Berry, Matthew M. “A Variable-Step Double-Integration Multi-Step Integrator.” 2004. Web. 31 Oct 2020.

Vancouver:

Berry MM. A Variable-Step Double-Integration Multi-Step Integrator. [Internet] [Doctoral dissertation]. Virginia Tech; 2004. [cited 2020 Oct 31]. Available from: http://hdl.handle.net/10919/11155.

Council of Science Editors:

Berry MM. A Variable-Step Double-Integration Multi-Step Integrator. [Doctoral Dissertation]. Virginia Tech; 2004. Available from: http://hdl.handle.net/10919/11155


Texas A&M University

5. Macomber, Brent David. Enhancements to Chebyshev-Picard Iteration Efficiency for Generally Perturbed Orbits and Constrained Dynamical Systems.

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

 Modified Chebyshev Picard Iteration (MCPI) is an iterative numerical method for solution of Ordinary Differential Equations (ODEs). This dissertation presents a body of work that… (more)

Subjects/Keywords: Numerical Methods; Ordinary Differential Equations; Parallel Computing; Orbit Propagation; Space Situational Awareness

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APA (6th Edition):

Macomber, B. D. (2015). Enhancements to Chebyshev-Picard Iteration Efficiency for Generally Perturbed Orbits and Constrained Dynamical Systems. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/155745

Chicago Manual of Style (16th Edition):

Macomber, Brent David. “Enhancements to Chebyshev-Picard Iteration Efficiency for Generally Perturbed Orbits and Constrained Dynamical Systems.” 2015. Doctoral Dissertation, Texas A&M University. Accessed October 31, 2020. http://hdl.handle.net/1969.1/155745.

MLA Handbook (7th Edition):

Macomber, Brent David. “Enhancements to Chebyshev-Picard Iteration Efficiency for Generally Perturbed Orbits and Constrained Dynamical Systems.” 2015. Web. 31 Oct 2020.

Vancouver:

Macomber BD. Enhancements to Chebyshev-Picard Iteration Efficiency for Generally Perturbed Orbits and Constrained Dynamical Systems. [Internet] [Doctoral dissertation]. Texas A&M University; 2015. [cited 2020 Oct 31]. Available from: http://hdl.handle.net/1969.1/155745.

Council of Science Editors:

Macomber BD. Enhancements to Chebyshev-Picard Iteration Efficiency for Generally Perturbed Orbits and Constrained Dynamical Systems. [Doctoral Dissertation]. Texas A&M University; 2015. Available from: http://hdl.handle.net/1969.1/155745


University of Oregon

6. Vitullo, Dashiell. Propagation of Photons through Optical Fiber: Spin-Orbit Interaction and Nonlinear Phase Modulation.

Degree: PhD, Department of Physics, 2016, University of Oregon

 We investigate two medium-facilitated interactions between properties of light upon propagation through optical fiber. The first is interaction between the spin and intrinsic orbital angular… (more)

Subjects/Keywords: Fiber optics; Nonlinear optics; Orbital angular momentum; Propagation; Quantum optics; Spin-orbit interaction

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APA (6th Edition):

Vitullo, D. (2016). Propagation of Photons through Optical Fiber: Spin-Orbit Interaction and Nonlinear Phase Modulation. (Doctoral Dissertation). University of Oregon. Retrieved from http://hdl.handle.net/1794/20708

Chicago Manual of Style (16th Edition):

Vitullo, Dashiell. “Propagation of Photons through Optical Fiber: Spin-Orbit Interaction and Nonlinear Phase Modulation.” 2016. Doctoral Dissertation, University of Oregon. Accessed October 31, 2020. http://hdl.handle.net/1794/20708.

MLA Handbook (7th Edition):

Vitullo, Dashiell. “Propagation of Photons through Optical Fiber: Spin-Orbit Interaction and Nonlinear Phase Modulation.” 2016. Web. 31 Oct 2020.

Vancouver:

Vitullo D. Propagation of Photons through Optical Fiber: Spin-Orbit Interaction and Nonlinear Phase Modulation. [Internet] [Doctoral dissertation]. University of Oregon; 2016. [cited 2020 Oct 31]. Available from: http://hdl.handle.net/1794/20708.

Council of Science Editors:

Vitullo D. Propagation of Photons through Optical Fiber: Spin-Orbit Interaction and Nonlinear Phase Modulation. [Doctoral Dissertation]. University of Oregon; 2016. Available from: http://hdl.handle.net/1794/20708

7. McCullough, Christopher Michael. Numerical integration accuracy and modeling for future geodetic missions.

Degree: MSin Engineering, Aerospace Engineering, 2013, University of Texas – Austin

 As technological advances throughout the field of satellite geodesy improve the accuracy of satellite measurements, numerical methods and algorithms must be able to keep pace.… (more)

Subjects/Keywords: GRACE; Numerical integration; Orbit propagation

…gravity field harmonics for 95 minute low Earth orbit… …orbit the Earth in a near circular and near polar orbit at an altitude of approximately 500… …orbit the Earth, they experience small accelerations due to the non-uniformity of the gravity… …satellite’s orbit to at least the nanometer per second level, the computed observations, y, will be… …accelerations imparted on the satellites while in orbit. These algorithms can be very simple, such as… 

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APA (6th Edition):

McCullough, C. M. (2013). Numerical integration accuracy and modeling for future geodetic missions. (Masters Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/21204

Chicago Manual of Style (16th Edition):

McCullough, Christopher Michael. “Numerical integration accuracy and modeling for future geodetic missions.” 2013. Masters Thesis, University of Texas – Austin. Accessed October 31, 2020. http://hdl.handle.net/2152/21204.

MLA Handbook (7th Edition):

McCullough, Christopher Michael. “Numerical integration accuracy and modeling for future geodetic missions.” 2013. Web. 31 Oct 2020.

Vancouver:

McCullough CM. Numerical integration accuracy and modeling for future geodetic missions. [Internet] [Masters thesis]. University of Texas – Austin; 2013. [cited 2020 Oct 31]. Available from: http://hdl.handle.net/2152/21204.

Council of Science Editors:

McCullough CM. Numerical integration accuracy and modeling for future geodetic missions. [Masters Thesis]. University of Texas – Austin; 2013. Available from: http://hdl.handle.net/2152/21204


Indian Institute of Science

8. Akila, S. Orbit Model Analysis And Dynamic Filter Compensation For Onboard Autonomy.

Degree: PhD, Faculty of Science, 2009, Indian Institute of Science

Orbit of a spacecraft in three dimensional Inertial Reference Frame is in general represented by a standard set of six parameters like Keplerian Orbital Elements… (more)

Subjects/Keywords: Orbit Models; Spacecraft Orbits; Dynamic Filters; Orbit Dynamics; Orbit Determination (OD); Orbit Propagation; Kalman Filter; Dynamics Filter Compensation (DFC); Astronautics

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APA (6th Edition):

Akila, S. (2009). Orbit Model Analysis And Dynamic Filter Compensation For Onboard Autonomy. (Doctoral Dissertation). Indian Institute of Science. Retrieved from http://etd.iisc.ac.in/handle/2005/398

Chicago Manual of Style (16th Edition):

Akila, S. “Orbit Model Analysis And Dynamic Filter Compensation For Onboard Autonomy.” 2009. Doctoral Dissertation, Indian Institute of Science. Accessed October 31, 2020. http://etd.iisc.ac.in/handle/2005/398.

MLA Handbook (7th Edition):

Akila, S. “Orbit Model Analysis And Dynamic Filter Compensation For Onboard Autonomy.” 2009. Web. 31 Oct 2020.

Vancouver:

Akila S. Orbit Model Analysis And Dynamic Filter Compensation For Onboard Autonomy. [Internet] [Doctoral dissertation]. Indian Institute of Science; 2009. [cited 2020 Oct 31]. Available from: http://etd.iisc.ac.in/handle/2005/398.

Council of Science Editors:

Akila S. Orbit Model Analysis And Dynamic Filter Compensation For Onboard Autonomy. [Doctoral Dissertation]. Indian Institute of Science; 2009. Available from: http://etd.iisc.ac.in/handle/2005/398


University of Colorado

9. Bradley, Ben K. Numerical Algorithms for Precise and Efficient Orbit Propagation and Positioning.

Degree: PhD, Aerospace Engineering Sciences, 2015, University of Colorado

  Motivated by the growing space catalog and the demands for precise orbit determination with shorter latency for science and reconnaissance missions, this research improves… (more)

Subjects/Keywords: Earth orientation parameters; International Terrestrial Reference System; Orbit propagation; Precise frame transformations; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

Bradley, B. K. (2015). Numerical Algorithms for Precise and Efficient Orbit Propagation and Positioning. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/125

Chicago Manual of Style (16th Edition):

Bradley, Ben K. “Numerical Algorithms for Precise and Efficient Orbit Propagation and Positioning.” 2015. Doctoral Dissertation, University of Colorado. Accessed October 31, 2020. https://scholar.colorado.edu/asen_gradetds/125.

MLA Handbook (7th Edition):

Bradley, Ben K. “Numerical Algorithms for Precise and Efficient Orbit Propagation and Positioning.” 2015. Web. 31 Oct 2020.

Vancouver:

Bradley BK. Numerical Algorithms for Precise and Efficient Orbit Propagation and Positioning. [Internet] [Doctoral dissertation]. University of Colorado; 2015. [cited 2020 Oct 31]. Available from: https://scholar.colorado.edu/asen_gradetds/125.

Council of Science Editors:

Bradley BK. Numerical Algorithms for Precise and Efficient Orbit Propagation and Positioning. [Doctoral Dissertation]. University of Colorado; 2015. Available from: https://scholar.colorado.edu/asen_gradetds/125

10. Reinthal, Eric. Relative Orbit Propagation and Control for Satellite Formation Flying using Continuous Low-thrust.

Degree: Electrical and Space Engineering, 2017, Luleå University of Technology

  For the upcoming formation flying technology demonstration mission NetSat a relative orbit propagator as well as a relative orbit controller were developed. The formation… (more)

Subjects/Keywords: formation flying; low-thrust; orbit propagation; control; continuous thrust; NetSat; electric propulsion; Aerospace Engineering; Rymd- och flygteknik

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APA (6th Edition):

Reinthal, E. (2017). Relative Orbit Propagation and Control for Satellite Formation Flying using Continuous Low-thrust. (Thesis). Luleå University of Technology. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-61664

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):

Reinthal, Eric. “Relative Orbit Propagation and Control for Satellite Formation Flying using Continuous Low-thrust.” 2017. Thesis, Luleå University of Technology. Accessed October 31, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-61664.

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

MLA Handbook (7th Edition):

Reinthal, Eric. “Relative Orbit Propagation and Control for Satellite Formation Flying using Continuous Low-thrust.” 2017. Web. 31 Oct 2020.

Vancouver:

Reinthal E. Relative Orbit Propagation and Control for Satellite Formation Flying using Continuous Low-thrust. [Internet] [Thesis]. Luleå University of Technology; 2017. [cited 2020 Oct 31]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-61664.

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

Council of Science Editors:

Reinthal E. Relative Orbit Propagation and Control for Satellite Formation Flying using Continuous Low-thrust. [Thesis]. Luleå University of Technology; 2017. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-61664

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


Delft University of Technology

11. Nardi, Alex (author). Orbit Modeling of Galilean Moons Flybys.

Degree: 2017, Delft University of Technology

 This research aims at modeling the trajectory followed by the Galileo spacecraft during a variety of flybys about the Galilean moons. The chosen flybys have… (more)

Subjects/Keywords: Galilean moons; Orbit modeling; Flyby; Hydrostaticity; Gravity field; Spherical harmonics; MATLAB; Integration; Propagation; Optimization; Data fitting

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APA (6th Edition):

Nardi, A. (. (2017). Orbit Modeling of Galilean Moons Flybys. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:38e13f1e-8424-4a00-bbad-70b9eadf97ac

Chicago Manual of Style (16th Edition):

Nardi, Alex (author). “Orbit Modeling of Galilean Moons Flybys.” 2017. Masters Thesis, Delft University of Technology. Accessed October 31, 2020. http://resolver.tudelft.nl/uuid:38e13f1e-8424-4a00-bbad-70b9eadf97ac.

MLA Handbook (7th Edition):

Nardi, Alex (author). “Orbit Modeling of Galilean Moons Flybys.” 2017. Web. 31 Oct 2020.

Vancouver:

Nardi A(. Orbit Modeling of Galilean Moons Flybys. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2020 Oct 31]. Available from: http://resolver.tudelft.nl/uuid:38e13f1e-8424-4a00-bbad-70b9eadf97ac.

Council of Science Editors:

Nardi A(. Orbit Modeling of Galilean Moons Flybys. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:38e13f1e-8424-4a00-bbad-70b9eadf97ac

12. Álvaro de Albuquerque Arraes. Propagation of uncertainties in the navigation of aerospace vehicles to minimize or maximize the collision risk.

Degree: 2008, Instituto Nacional de Pesquisas Espaciais

Neste trabalho realizou-se o estudo de diversas idéias relacionadas ao problema do cálculo de probabilidade de colisão de satélites. Com base nessas idéias, foi realizada… (more)

Subjects/Keywords: formação de satélites; estimação de trajetória; propagação de matriz de covariancia; detritos espaciais; collision avoidance; satellite formation flying; orbit prediction; covariance propagation; debris; elisão de colisão

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APA (6th Edition):

Arraes, . d. A. (2008). Propagation of uncertainties in the navigation of aerospace vehicles to minimize or maximize the collision risk. (Thesis). Instituto Nacional de Pesquisas Espaciais. Retrieved from http://urlib.net/sid.inpe.br/[email protected]/2008/10.14.00.42

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):

Arraes, Álvaro de Albuquerque. “Propagation of uncertainties in the navigation of aerospace vehicles to minimize or maximize the collision risk.” 2008. Thesis, Instituto Nacional de Pesquisas Espaciais. Accessed October 31, 2020. http://urlib.net/sid.inpe.br/[email protected]/2008/10.14.00.42.

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

MLA Handbook (7th Edition):

Arraes, Álvaro de Albuquerque. “Propagation of uncertainties in the navigation of aerospace vehicles to minimize or maximize the collision risk.” 2008. Web. 31 Oct 2020.

Vancouver:

Arraes dA. Propagation of uncertainties in the navigation of aerospace vehicles to minimize or maximize the collision risk. [Internet] [Thesis]. Instituto Nacional de Pesquisas Espaciais; 2008. [cited 2020 Oct 31]. Available from: http://urlib.net/sid.inpe.br/[email protected]/2008/10.14.00.42.

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

Council of Science Editors:

Arraes dA. Propagation of uncertainties in the navigation of aerospace vehicles to minimize or maximize the collision risk. [Thesis]. Instituto Nacional de Pesquisas Espaciais; 2008. Available from: http://urlib.net/sid.inpe.br/[email protected]/2008/10.14.00.42

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

13. Puglisi, Alessandra. Ab-initio study of x-ray spectroscopy of molecular ions : Calculs ab-initio des spectre de photoabsorption X d'ions moléculaires.

Degree: Docteur es, Chimie physique et Chimie analytique, 2017, Université Pierre et Marie Curie – Paris VI

La signature spectroscopique des ions moléculaires est fondamentale pour l'étude et la caractérisation de plasma en astrophysique et en laboratoire. Différentes techniques peuvent être utilisées… (more)

Subjects/Keywords: Calculs ab-Initio; Interaction de configuration; Propagation du paquet d'onde; Spectroscopie à rayon-X; Couplage spin-Orbite; Ions moléculaires; Ab-initio calculations; X-ray photoabsorption spectroscopy; Spin-orbit coupling; 541.3

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APA (6th Edition):

Puglisi, A. (2017). Ab-initio study of x-ray spectroscopy of molecular ions : Calculs ab-initio des spectre de photoabsorption X d'ions moléculaires. (Doctoral Dissertation). Université Pierre et Marie Curie – Paris VI. Retrieved from http://www.theses.fr/2017PA066257

Chicago Manual of Style (16th Edition):

Puglisi, Alessandra. “Ab-initio study of x-ray spectroscopy of molecular ions : Calculs ab-initio des spectre de photoabsorption X d'ions moléculaires.” 2017. Doctoral Dissertation, Université Pierre et Marie Curie – Paris VI. Accessed October 31, 2020. http://www.theses.fr/2017PA066257.

MLA Handbook (7th Edition):

Puglisi, Alessandra. “Ab-initio study of x-ray spectroscopy of molecular ions : Calculs ab-initio des spectre de photoabsorption X d'ions moléculaires.” 2017. Web. 31 Oct 2020.

Vancouver:

Puglisi A. Ab-initio study of x-ray spectroscopy of molecular ions : Calculs ab-initio des spectre de photoabsorption X d'ions moléculaires. [Internet] [Doctoral dissertation]. Université Pierre et Marie Curie – Paris VI; 2017. [cited 2020 Oct 31]. Available from: http://www.theses.fr/2017PA066257.

Council of Science Editors:

Puglisi A. Ab-initio study of x-ray spectroscopy of molecular ions : Calculs ab-initio des spectre de photoabsorption X d'ions moléculaires. [Doctoral Dissertation]. Université Pierre et Marie Curie – Paris VI; 2017. Available from: http://www.theses.fr/2017PA066257


University of Houston

14. Nallapu, Raviteja 1989-. Orbit Propagation via MRQ Sphere Technique.

Degree: MS, Aerospace Engineering, 2012, University of Houston

 The Multi-Resolution Quadrature (MRQ) Sphere model, is a newly developed multi- resolution gravity model designed to estimate the gravity fields of arbitrary shaped space bodies,… (more)

Subjects/Keywords: Orbit Propagation; Gravity Estimation; MRQ-Sphere; Spherical harmonics; LAGEOS-II; GPS BIIA-10; Cartesian Formulation; Kepplerian elements; Gravity Potential; Orbital Mechanics; Aerospace engineering

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APA (6th Edition):

Nallapu, R. 1. (2012). Orbit Propagation via MRQ Sphere Technique. (Masters Thesis). University of Houston. Retrieved from http://hdl.handle.net/10657/765

Chicago Manual of Style (16th Edition):

Nallapu, Raviteja 1989-. “Orbit Propagation via MRQ Sphere Technique.” 2012. Masters Thesis, University of Houston. Accessed October 31, 2020. http://hdl.handle.net/10657/765.

MLA Handbook (7th Edition):

Nallapu, Raviteja 1989-. “Orbit Propagation via MRQ Sphere Technique.” 2012. Web. 31 Oct 2020.

Vancouver:

Nallapu R1. Orbit Propagation via MRQ Sphere Technique. [Internet] [Masters thesis]. University of Houston; 2012. [cited 2020 Oct 31]. Available from: http://hdl.handle.net/10657/765.

Council of Science Editors:

Nallapu R1. Orbit Propagation via MRQ Sphere Technique. [Masters Thesis]. University of Houston; 2012. Available from: http://hdl.handle.net/10657/765


University of Washington

15. Awad, Armand Issam. Advances and Applications of Multiple Scale Methods in Complex Dynamical Systems.

Degree: PhD, 2017, University of Washington

 High dimensionality, numerical stiffness, and complex subsystem interactions pose fundamental challenges for the design, analysis, and certification of modern aerospace systems. This dissertation addresses these… (more)

Subjects/Keywords: Hybrid Systems; Multiple Timescales; Networked Dynamical Systems; Orbit Propagation; Reduced-Order Modelling; Singular Perturbation Theory; Aerospace engineering; Applied mathematics; Aeronautics and astronautics

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

APA (6th Edition):

Awad, A. I. (2017). Advances and Applications of Multiple Scale Methods in Complex Dynamical Systems. (Doctoral Dissertation). University of Washington. Retrieved from http://hdl.handle.net/1773/39920

Chicago Manual of Style (16th Edition):

Awad, Armand Issam. “Advances and Applications of Multiple Scale Methods in Complex Dynamical Systems.” 2017. Doctoral Dissertation, University of Washington. Accessed October 31, 2020. http://hdl.handle.net/1773/39920.

MLA Handbook (7th Edition):

Awad, Armand Issam. “Advances and Applications of Multiple Scale Methods in Complex Dynamical Systems.” 2017. Web. 31 Oct 2020.

Vancouver:

Awad AI. Advances and Applications of Multiple Scale Methods in Complex Dynamical Systems. [Internet] [Doctoral dissertation]. University of Washington; 2017. [cited 2020 Oct 31]. Available from: http://hdl.handle.net/1773/39920.

Council of Science Editors:

Awad AI. Advances and Applications of Multiple Scale Methods in Complex Dynamical Systems. [Doctoral Dissertation]. University of Washington; 2017. Available from: http://hdl.handle.net/1773/39920

16. Locke, Travis Cole. Further Developments in Orbit Ephemeris Derived Neutral Density.

Degree: MS, Aerospace Engineering, 2012, University of Kansas

 There are a number of non-conservative forces acting on a satellite in low Earth orbit. The one which is the most dominant and also contains… (more)

Subjects/Keywords: Aerospace engineering; Engineering; Density; Ephemeris; Orbit determination; Propagation

…variations in the orbit propagation process. The effects of varying levels of noise being present… …Ranging Service LEO Low Earth Orbit Mass Spectrometer Incoherent Scatter Extending from ground… …Mass Spectrometer Incoherent Scatter NRLMSISE Extending from ground to space ODTK Orbit… …Determination Tool Kit POE Precision Orbit Ephemerides xi PSO Precision Science Orbit RMS Root… …Mean Square RSO Rapid Science Orbit SETA Satellite Electrostatic Triaxial Accelerometer… 

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

APA (6th Edition):

Locke, T. C. (2012). Further Developments in Orbit Ephemeris Derived Neutral Density. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/10617

Chicago Manual of Style (16th Edition):

Locke, Travis Cole. “Further Developments in Orbit Ephemeris Derived Neutral Density.” 2012. Masters Thesis, University of Kansas. Accessed October 31, 2020. http://hdl.handle.net/1808/10617.

MLA Handbook (7th Edition):

Locke, Travis Cole. “Further Developments in Orbit Ephemeris Derived Neutral Density.” 2012. Web. 31 Oct 2020.

Vancouver:

Locke TC. Further Developments in Orbit Ephemeris Derived Neutral Density. [Internet] [Masters thesis]. University of Kansas; 2012. [cited 2020 Oct 31]. Available from: http://hdl.handle.net/1808/10617.

Council of Science Editors:

Locke TC. Further Developments in Orbit Ephemeris Derived Neutral Density. [Masters Thesis]. University of Kansas; 2012. Available from: http://hdl.handle.net/1808/10617


Cal Poly

17. Miura, Nicholas Z. COMPARISON AND DESIGN OF SIMPLIFIED GENERAL PERTURBATION MODELS (SGP4) AND CODE FOR NASA JOHNSON SPACE CENTER, ORBITAL DEBRIS PROGRAM OFFICE.

Degree: MS, Aerospace Engineering, 2009, Cal Poly

 This graduate project compares legacy simplified general perturbation model (SGP4) code developed by NASA Johnson Space Center, Orbital Debris Program Office, to a recent public… (more)

Subjects/Keywords: SGP4; Orbit Propagation; Vallado; Astrodynamics; Navigation, Guidance, Control and Dynamics; Systems Engineering and Multidisciplinary Design Optimization

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

APA (6th Edition):

Miura, N. Z. (2009). COMPARISON AND DESIGN OF SIMPLIFIED GENERAL PERTURBATION MODELS (SGP4) AND CODE FOR NASA JOHNSON SPACE CENTER, ORBITAL DEBRIS PROGRAM OFFICE. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/86 ; 10.15368/theses.2009.55

Chicago Manual of Style (16th Edition):

Miura, Nicholas Z. “COMPARISON AND DESIGN OF SIMPLIFIED GENERAL PERTURBATION MODELS (SGP4) AND CODE FOR NASA JOHNSON SPACE CENTER, ORBITAL DEBRIS PROGRAM OFFICE.” 2009. Masters Thesis, Cal Poly. Accessed October 31, 2020. https://digitalcommons.calpoly.edu/theses/86 ; 10.15368/theses.2009.55.

MLA Handbook (7th Edition):

Miura, Nicholas Z. “COMPARISON AND DESIGN OF SIMPLIFIED GENERAL PERTURBATION MODELS (SGP4) AND CODE FOR NASA JOHNSON SPACE CENTER, ORBITAL DEBRIS PROGRAM OFFICE.” 2009. Web. 31 Oct 2020.

Vancouver:

Miura NZ. COMPARISON AND DESIGN OF SIMPLIFIED GENERAL PERTURBATION MODELS (SGP4) AND CODE FOR NASA JOHNSON SPACE CENTER, ORBITAL DEBRIS PROGRAM OFFICE. [Internet] [Masters thesis]. Cal Poly; 2009. [cited 2020 Oct 31]. Available from: https://digitalcommons.calpoly.edu/theses/86 ; 10.15368/theses.2009.55.

Council of Science Editors:

Miura NZ. COMPARISON AND DESIGN OF SIMPLIFIED GENERAL PERTURBATION MODELS (SGP4) AND CODE FOR NASA JOHNSON SPACE CENTER, ORBITAL DEBRIS PROGRAM OFFICE. [Masters Thesis]. Cal Poly; 2009. Available from: https://digitalcommons.calpoly.edu/theses/86 ; 10.15368/theses.2009.55

18. Dykstra, Matthew C. Single station Doppler tracking for satellite orbit prediction and propagation.

Degree: MSin Engineering, Aerospace Engineering, 2015, University of Texas – Austin

 Presently, there are two main methods of launching a cube satellite into Earth orbit. The first method is to purchase a secondary payload slot on… (more)

Subjects/Keywords: Satellite; Propagation; Doppler; Tracking; Estimation; CubeSat; Ground station; Orbit; Prediction; Scheduling; Reference frame

orbit propagation, alone will result in errors on the order of a few kilometers to tens of… …tracking and orbit propagation. 3.1 Reference Frames There are a number of necessary reference… …Case Selection . . . . . . . 7.1.2 Orbit Prediction Results . . . . 7.2 Pass Selection and… …Nominal State Selection 7.3.3 Orbit Prediction Results… …Graphical representation of the orbital elements for a typical orbit[13]. Graphical… 

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

APA (6th Edition):

Dykstra, M. C. (2015). Single station Doppler tracking for satellite orbit prediction and propagation. (Masters Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/31713

Chicago Manual of Style (16th Edition):

Dykstra, Matthew C. “Single station Doppler tracking for satellite orbit prediction and propagation.” 2015. Masters Thesis, University of Texas – Austin. Accessed October 31, 2020. http://hdl.handle.net/2152/31713.

MLA Handbook (7th Edition):

Dykstra, Matthew C. “Single station Doppler tracking for satellite orbit prediction and propagation.” 2015. Web. 31 Oct 2020.

Vancouver:

Dykstra MC. Single station Doppler tracking for satellite orbit prediction and propagation. [Internet] [Masters thesis]. University of Texas – Austin; 2015. [cited 2020 Oct 31]. Available from: http://hdl.handle.net/2152/31713.

Council of Science Editors:

Dykstra MC. Single station Doppler tracking for satellite orbit prediction and propagation. [Masters Thesis]. University of Texas – Austin; 2015. Available from: http://hdl.handle.net/2152/31713


Indian Institute of Science

19. Nagarajan, N. Autonomous Orbit Estimation For Near Earth Satellites Using Horizon Scanners.

Degree: PhD, Faculty of Engineering, 2005, Indian Institute of Science

 Autonomous navigation is the determination of satellites position and velocity vectors onboard the satellite, using the measurements available onboard. The orbital information of a satellite… (more)

Subjects/Keywords: Astronautics; Artificial Satellites - Orbits; Horizon Sensing; Horizon Sensor; Orbit Determination; Horizon Unit Vectors; Low Pass Filter (LPF); Autonomous Orbit Determination; Augmented State Filter; Orbit Propagation; Earth oblateness; Low Eccentricityn Orbits; Horizon Points; Autonomous Navigation; Extended Kalman Filter; Kalman filtering

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

APA (6th Edition):

Nagarajan, N. (2005). Autonomous Orbit Estimation For Near Earth Satellites Using Horizon Scanners. (Doctoral Dissertation). Indian Institute of Science. Retrieved from http://etd.iisc.ac.in/handle/2005/155

Chicago Manual of Style (16th Edition):

Nagarajan, N. “Autonomous Orbit Estimation For Near Earth Satellites Using Horizon Scanners.” 2005. Doctoral Dissertation, Indian Institute of Science. Accessed October 31, 2020. http://etd.iisc.ac.in/handle/2005/155.

MLA Handbook (7th Edition):

Nagarajan, N. “Autonomous Orbit Estimation For Near Earth Satellites Using Horizon Scanners.” 2005. Web. 31 Oct 2020.

Vancouver:

Nagarajan N. Autonomous Orbit Estimation For Near Earth Satellites Using Horizon Scanners. [Internet] [Doctoral dissertation]. Indian Institute of Science; 2005. [cited 2020 Oct 31]. Available from: http://etd.iisc.ac.in/handle/2005/155.

Council of Science Editors:

Nagarajan N. Autonomous Orbit Estimation For Near Earth Satellites Using Horizon Scanners. [Doctoral Dissertation]. Indian Institute of Science; 2005. Available from: http://etd.iisc.ac.in/handle/2005/155

20. Leary, Cody Collin, 1981-. Measurement and control of transverse photonic degrees of freedom via parity sorting and spin-orbit interaction.

Degree: 2010, University of Oregon

 In this dissertation, several new methods for the measurement and control of transverse photonic degrees of freedom are developed. We demonstrate a mode sorter for… (more)

Subjects/Keywords: Degrees of freedom; Spin orbit interactions; Parity sorting; Geometric phases; Transverse spacial modes; Photon propagation; Quantum physics; Optics; Particle physics

…147 ... . . . . . . . . . . . . .. Spin-Orbit Correction to the Propagation Constant… …Spin-Orbit Wave Packet in a Weakly Inhomogeneous Medium 18 Geometric Phase of a General… …a Spin-Orbit Wave Packet… …Modes. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. 107 110 V. SPIN-ORBIT… …113 Spin-Orbit Wave Equations… 

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

APA (6th Edition):

Leary, Cody Collin, 1. (2010). Measurement and control of transverse photonic degrees of freedom via parity sorting and spin-orbit interaction. (Thesis). University of Oregon. Retrieved from http://hdl.handle.net/1794/10910

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):

Leary, Cody Collin, 1981-. “Measurement and control of transverse photonic degrees of freedom via parity sorting and spin-orbit interaction.” 2010. Thesis, University of Oregon. Accessed October 31, 2020. http://hdl.handle.net/1794/10910.

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

MLA Handbook (7th Edition):

Leary, Cody Collin, 1981-. “Measurement and control of transverse photonic degrees of freedom via parity sorting and spin-orbit interaction.” 2010. Web. 31 Oct 2020.

Vancouver:

Leary, Cody Collin 1. Measurement and control of transverse photonic degrees of freedom via parity sorting and spin-orbit interaction. [Internet] [Thesis]. University of Oregon; 2010. [cited 2020 Oct 31]. Available from: http://hdl.handle.net/1794/10910.

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

Council of Science Editors:

Leary, Cody Collin 1. Measurement and control of transverse photonic degrees of freedom via parity sorting and spin-orbit interaction. [Thesis]. University of Oregon; 2010. Available from: http://hdl.handle.net/1794/10910

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


Pontifical Catholic University of Rio de Janeiro

21. MARTA PUDWELL CHAVES DE ALMEIDA. [en] PROPAGATION EFFECTS IN LOW EARTH ORBIT SATTELITE LINKS.

Degree: 2003, Pontifical Catholic University of Rio de Janeiro

[pt] O efeito da atenuação por chuvas em enlaces satélites que operam em frequências acima de 10 GHz é decisivo no cálculo de desempenho do… (more)

Subjects/Keywords: [pt] PROPAGACAO DE ONDAS; [en] WAVE PROPAGATION; [pt] ATENUACAO POR CHUVAS; [en] RAIN ATTENUATION; [pt] ENLACES SATELITE; [en] SATELLITE LINKS; [pt] ORBITA DE SATELITES GEOESTACIONARIOS; [en] GEOESTATIONARY SATELLITE ORBIT; [pt] PRECIPITACAO; [en] PRECIPITATION; [pt] SISTEMA DE ORBITA BAIXA; [en] LOW ORBIT SYSTEM

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APA (6th Edition):

ALMEIDA, M. P. C. D. (2003). [en] PROPAGATION EFFECTS IN LOW EARTH ORBIT SATTELITE LINKS. (Thesis). Pontifical Catholic University of Rio de Janeiro. Retrieved from http://www.maxwell.vrac.puc-rio.br/Busca_etds.php?strSecao=resultado&nrSeq=4245

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):

ALMEIDA, MARTA PUDWELL CHAVES DE. “[en] PROPAGATION EFFECTS IN LOW EARTH ORBIT SATTELITE LINKS.” 2003. Thesis, Pontifical Catholic University of Rio de Janeiro. Accessed October 31, 2020. http://www.maxwell.vrac.puc-rio.br/Busca_etds.php?strSecao=resultado&nrSeq=4245.

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

MLA Handbook (7th Edition):

ALMEIDA, MARTA PUDWELL CHAVES DE. “[en] PROPAGATION EFFECTS IN LOW EARTH ORBIT SATTELITE LINKS.” 2003. Web. 31 Oct 2020.

Vancouver:

ALMEIDA MPCD. [en] PROPAGATION EFFECTS IN LOW EARTH ORBIT SATTELITE LINKS. [Internet] [Thesis]. Pontifical Catholic University of Rio de Janeiro; 2003. [cited 2020 Oct 31]. Available from: http://www.maxwell.vrac.puc-rio.br/Busca_etds.php?strSecao=resultado&nrSeq=4245.

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

Council of Science Editors:

ALMEIDA MPCD. [en] PROPAGATION EFFECTS IN LOW EARTH ORBIT SATTELITE LINKS. [Thesis]. Pontifical Catholic University of Rio de Janeiro; 2003. Available from: http://www.maxwell.vrac.puc-rio.br/Busca_etds.php?strSecao=resultado&nrSeq=4245

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


Indian Institute of Science

22. Anilkumar, A K. NEW PERSPECTIVES FOR ANALYZING THE BREAKUP, ENVIRONMENT, EVOLUTION, COLLISION RISK AND REENTRY OF SPACE DEBRIS OBJECTS.

Degree: PhD, Faculty of Engineering, 2005, Indian Institute of Science

 In the space surrounding the earth there are two major regions where orbital debris causes concern. They are the Low Earth Orbits (LEO) up to… (more)

Subjects/Keywords: Aerospace Engineering; Space Debris Modelling; On Orbit Breakup; Debris Clouds; Evolution; Collision Risk; Re entry; Kalman Filter; ASSEMBLE Model; SIMPLE model; Orbital Elements; Propagation; Collision probability; Semi major axis

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

APA (6th Edition):

Anilkumar, A. K. (2005). NEW PERSPECTIVES FOR ANALYZING THE BREAKUP, ENVIRONMENT, EVOLUTION, COLLISION RISK AND REENTRY OF SPACE DEBRIS OBJECTS. (Doctoral Dissertation). Indian Institute of Science. Retrieved from http://etd.iisc.ac.in/handle/2005/80

Chicago Manual of Style (16th Edition):

Anilkumar, A K. “NEW PERSPECTIVES FOR ANALYZING THE BREAKUP, ENVIRONMENT, EVOLUTION, COLLISION RISK AND REENTRY OF SPACE DEBRIS OBJECTS.” 2005. Doctoral Dissertation, Indian Institute of Science. Accessed October 31, 2020. http://etd.iisc.ac.in/handle/2005/80.

MLA Handbook (7th Edition):

Anilkumar, A K. “NEW PERSPECTIVES FOR ANALYZING THE BREAKUP, ENVIRONMENT, EVOLUTION, COLLISION RISK AND REENTRY OF SPACE DEBRIS OBJECTS.” 2005. Web. 31 Oct 2020.

Vancouver:

Anilkumar AK. NEW PERSPECTIVES FOR ANALYZING THE BREAKUP, ENVIRONMENT, EVOLUTION, COLLISION RISK AND REENTRY OF SPACE DEBRIS OBJECTS. [Internet] [Doctoral dissertation]. Indian Institute of Science; 2005. [cited 2020 Oct 31]. Available from: http://etd.iisc.ac.in/handle/2005/80.

Council of Science Editors:

Anilkumar AK. NEW PERSPECTIVES FOR ANALYZING THE BREAKUP, ENVIRONMENT, EVOLUTION, COLLISION RISK AND REENTRY OF SPACE DEBRIS OBJECTS. [Doctoral Dissertation]. Indian Institute of Science; 2005. Available from: http://etd.iisc.ac.in/handle/2005/80

.