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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

URL: https://scholar.colorado.edu/asen_gradetds/11

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: https://submit-etda.libraries.psu.edu/catalog/29463

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

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

URL: http://resolver.tudelft.nl/uuid:f550d59a-7d15-46dd-a084-025ace46e643

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/10919/11155

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/1969.1/155745

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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-

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

URL: http://hdl.handle.net/1794/20708

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/2152/21204

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://etd.iisc.ac.in/handle/2005/398

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

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: https://scholar.colorado.edu/asen_gradetds/125

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

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-61664

► 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 (6^{th} 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

Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^{th} 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.

Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^{th} 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.

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

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

URL: http://resolver.tudelft.nl/uuid:38e13f1e-8424-4a00-bbad-70b9eadf97ac

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://urlib.net/sid.inpe.br/[email protected]/2008/10.14.00.42

►

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 (6^{th} 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

Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^{th} 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.

Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^{th} 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.

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

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

URL: http://www.theses.fr/2017PA066257

►

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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/10657/765

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/1773/39920

► 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

Record Details Similar Records

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

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/1808/10617

► 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…

Record Details Similar Records

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

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: https://digitalcommons.calpoly.edu/theses/86 ; 10.15368/theses.2009.55

► 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

Record Details Similar Records

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

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/2152/31713

► 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…

Record Details Similar Records

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

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://etd.iisc.ac.in/handle/2005/155

► 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

Record Details Similar Records

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

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/1794/10910

► 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…

Record Details Similar Records

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

APA (6^{th} 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

Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^{th} 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.

Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^{th} 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.

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

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

URL: http://www.maxwell.vrac.puc-rio.br/Busca_etds.php?strSecao=resultado&nrSeq=4245

►

[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

Record Details Similar Records

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

APA (6^{th} 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

Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^{th} 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.

Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^{th} 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.

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

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

URL: http://etd.iisc.ac.in/handle/2005/80

► 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

Record Details Similar Records

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

APA (6^{th} 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 (16^{th} 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 (7^{th} 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