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You searched for subject:(astrodynamics). Showing records 1 – 30 of 109 total matches.

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Embry-Riddle Aeronautical University

1. Iyengar, Spatika Dasharati. Computation of Hypersonic Flows with Lateral Jets Using k-ω Turbulence Model.

Degree: MSin Aerospace Engineering, Graduate Studies, 2015, Embry-Riddle Aeronautical University

  Thermal Protection systems (TPS) are used as shields in space vehicles which encounter high heat and temperatures at the reentry altitudes. Among them, the… (more)

Subjects/Keywords: Astrodynamics

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APA (6th Edition):

Iyengar, S. D. (2015). Computation of Hypersonic Flows with Lateral Jets Using k-ω Turbulence Model. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from http://commons.erau.edu/edt/251

Chicago Manual of Style (16th Edition):

Iyengar, Spatika Dasharati. “Computation of Hypersonic Flows with Lateral Jets Using k-ω Turbulence Model.” 2015. Masters Thesis, Embry-Riddle Aeronautical University. Accessed December 14, 2019. http://commons.erau.edu/edt/251.

MLA Handbook (7th Edition):

Iyengar, Spatika Dasharati. “Computation of Hypersonic Flows with Lateral Jets Using k-ω Turbulence Model.” 2015. Web. 14 Dec 2019.

Vancouver:

Iyengar SD. Computation of Hypersonic Flows with Lateral Jets Using k-ω Turbulence Model. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2015. [cited 2019 Dec 14]. Available from: http://commons.erau.edu/edt/251.

Council of Science Editors:

Iyengar SD. Computation of Hypersonic Flows with Lateral Jets Using k-ω Turbulence Model. [Masters Thesis]. Embry-Riddle Aeronautical University; 2015. Available from: http://commons.erau.edu/edt/251


Embry-Riddle Aeronautical University

2. Sestak, Timothy Allen. The Effect of Surface Materials and Morphology on Wingsuit Aerodynamics.

Degree: PhD, College of Aviation, 2017, Embry-Riddle Aeronautical University

  This study examines the aerodynamic effects of the materials, textiles, and morphologies currently used in wingsuit design and construction. The experiment was a low-speed… (more)

Subjects/Keywords: Astrodynamics; Aviation

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APA (6th Edition):

Sestak, T. A. (2017). The Effect of Surface Materials and Morphology on Wingsuit Aerodynamics. (Doctoral Dissertation). Embry-Riddle Aeronautical University. Retrieved from http://commons.erau.edu/edt/355

Chicago Manual of Style (16th Edition):

Sestak, Timothy Allen. “The Effect of Surface Materials and Morphology on Wingsuit Aerodynamics.” 2017. Doctoral Dissertation, Embry-Riddle Aeronautical University. Accessed December 14, 2019. http://commons.erau.edu/edt/355.

MLA Handbook (7th Edition):

Sestak, Timothy Allen. “The Effect of Surface Materials and Morphology on Wingsuit Aerodynamics.” 2017. Web. 14 Dec 2019.

Vancouver:

Sestak TA. The Effect of Surface Materials and Morphology on Wingsuit Aerodynamics. [Internet] [Doctoral dissertation]. Embry-Riddle Aeronautical University; 2017. [cited 2019 Dec 14]. Available from: http://commons.erau.edu/edt/355.

Council of Science Editors:

Sestak TA. The Effect of Surface Materials and Morphology on Wingsuit Aerodynamics. [Doctoral Dissertation]. Embry-Riddle Aeronautical University; 2017. Available from: http://commons.erau.edu/edt/355

3. Vittaldev, V. The Unified State Model. Derivation and Applications in Astrodynamics and Navigation.:.

Degree: 2010, Delft University of Technology

Subjects/Keywords: Astrodynamics

…13 14 16 17 19 20 21 21 22 23 24 4 Astrodynamics and Orbital Mechanics 4.1 Gravity… …of astrodynamics and the space environment with the various perturbations… 

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APA (6th Edition):

Vittaldev, V. (2010). The Unified State Model. Derivation and Applications in Astrodynamics and Navigation.:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:198390b8-b81f-4a13-9c80-15befd3c0428

Chicago Manual of Style (16th Edition):

Vittaldev, V. “The Unified State Model. Derivation and Applications in Astrodynamics and Navigation.:.” 2010. Masters Thesis, Delft University of Technology. Accessed December 14, 2019. http://resolver.tudelft.nl/uuid:198390b8-b81f-4a13-9c80-15befd3c0428.

MLA Handbook (7th Edition):

Vittaldev, V. “The Unified State Model. Derivation and Applications in Astrodynamics and Navigation.:.” 2010. Web. 14 Dec 2019.

Vancouver:

Vittaldev V. The Unified State Model. Derivation and Applications in Astrodynamics and Navigation.:. [Internet] [Masters thesis]. Delft University of Technology; 2010. [cited 2019 Dec 14]. Available from: http://resolver.tudelft.nl/uuid:198390b8-b81f-4a13-9c80-15befd3c0428.

Council of Science Editors:

Vittaldev V. The Unified State Model. Derivation and Applications in Astrodynamics and Navigation.:. [Masters Thesis]. Delft University of Technology; 2010. Available from: http://resolver.tudelft.nl/uuid:198390b8-b81f-4a13-9c80-15befd3c0428


Cal Poly

4. Farahmand, Mitra. ORBITAL PROPAGATORS FOR HORIZON SIMULATION FRAMEWORK.

Degree: MS, Aerospace Engineering, 2009, Cal Poly

 This thesis describes the models of four common orbital propagators and outlines the process of integrating them into the Horizon Simulation Framework (HSF). The results… (more)

Subjects/Keywords: Astrodynamics

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APA (6th Edition):

Farahmand, M. (2009). ORBITAL PROPAGATORS FOR HORIZON SIMULATION FRAMEWORK. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/167 ; 10.15368/theses.2009.138

Chicago Manual of Style (16th Edition):

Farahmand, Mitra. “ORBITAL PROPAGATORS FOR HORIZON SIMULATION FRAMEWORK.” 2009. Masters Thesis, Cal Poly. Accessed December 14, 2019. https://digitalcommons.calpoly.edu/theses/167 ; 10.15368/theses.2009.138.

MLA Handbook (7th Edition):

Farahmand, Mitra. “ORBITAL PROPAGATORS FOR HORIZON SIMULATION FRAMEWORK.” 2009. Web. 14 Dec 2019.

Vancouver:

Farahmand M. ORBITAL PROPAGATORS FOR HORIZON SIMULATION FRAMEWORK. [Internet] [Masters thesis]. Cal Poly; 2009. [cited 2019 Dec 14]. Available from: https://digitalcommons.calpoly.edu/theses/167 ; 10.15368/theses.2009.138.

Council of Science Editors:

Farahmand M. ORBITAL PROPAGATORS FOR HORIZON SIMULATION FRAMEWORK. [Masters Thesis]. Cal Poly; 2009. Available from: https://digitalcommons.calpoly.edu/theses/167 ; 10.15368/theses.2009.138


Purdue University

5. Haapala, Amanda F. Trajectory design in the spatial circular restricted three-body problem exploiting higher-dimensional Poincare maps.

Degree: PhD, Aeronautics and Astronautics, 2014, Purdue University

  In this investigation, the role of higher-dimensional Poincaré maps in facilitating trajectory design is explored for a variety of applications. To begin, existing strategies… (more)

Subjects/Keywords: Aerospace Engineering; Astrodynamics

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APA (6th Edition):

Haapala, A. F. (2014). Trajectory design in the spatial circular restricted three-body problem exploiting higher-dimensional Poincare maps. (Doctoral Dissertation). Purdue University. Retrieved from https://docs.lib.purdue.edu/open_access_dissertations/278

Chicago Manual of Style (16th Edition):

Haapala, Amanda F. “Trajectory design in the spatial circular restricted three-body problem exploiting higher-dimensional Poincare maps.” 2014. Doctoral Dissertation, Purdue University. Accessed December 14, 2019. https://docs.lib.purdue.edu/open_access_dissertations/278.

MLA Handbook (7th Edition):

Haapala, Amanda F. “Trajectory design in the spatial circular restricted three-body problem exploiting higher-dimensional Poincare maps.” 2014. Web. 14 Dec 2019.

Vancouver:

Haapala AF. Trajectory design in the spatial circular restricted three-body problem exploiting higher-dimensional Poincare maps. [Internet] [Doctoral dissertation]. Purdue University; 2014. [cited 2019 Dec 14]. Available from: https://docs.lib.purdue.edu/open_access_dissertations/278.

Council of Science Editors:

Haapala AF. Trajectory design in the spatial circular restricted three-body problem exploiting higher-dimensional Poincare maps. [Doctoral Dissertation]. Purdue University; 2014. Available from: https://docs.lib.purdue.edu/open_access_dissertations/278


Cal Poly

6. Strange, Michael R. Orbital Determination Feasibility of LEO Nanosatellites Using Small Aperture Telescopes.

Degree: MS, Aerospace Engineering, 2017, Cal Poly

  This thesis is directed toward the feasibility of observing satellites on the nano scale and determining an accurate propagated orbit using a Meade LX600-ACF… (more)

Subjects/Keywords: observation; satellite; propogation; Astrodynamics

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APA (6th Edition):

Strange, M. R. (2017). Orbital Determination Feasibility of LEO Nanosatellites Using Small Aperture Telescopes. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1714

Chicago Manual of Style (16th Edition):

Strange, Michael R. “Orbital Determination Feasibility of LEO Nanosatellites Using Small Aperture Telescopes.” 2017. Masters Thesis, Cal Poly. Accessed December 14, 2019. https://digitalcommons.calpoly.edu/theses/1714.

MLA Handbook (7th Edition):

Strange, Michael R. “Orbital Determination Feasibility of LEO Nanosatellites Using Small Aperture Telescopes.” 2017. Web. 14 Dec 2019.

Vancouver:

Strange MR. Orbital Determination Feasibility of LEO Nanosatellites Using Small Aperture Telescopes. [Internet] [Masters thesis]. Cal Poly; 2017. [cited 2019 Dec 14]. Available from: https://digitalcommons.calpoly.edu/theses/1714.

Council of Science Editors:

Strange MR. Orbital Determination Feasibility of LEO Nanosatellites Using Small Aperture Telescopes. [Masters Thesis]. Cal Poly; 2017. Available from: https://digitalcommons.calpoly.edu/theses/1714


Embry-Riddle Aeronautical University

7. Coulter, Nolan. Design of an Attitude Control System for a Spacecraft with Propellant Slosh Dynamics.

Degree: MSin Aerospace Engineering, Graduate Studies, 2018, Embry-Riddle Aeronautical University

  The presence of propellant slosh dynamics in a spacecraft system during a maneuver leads to attitude control system (ACS) performance degradation resulting in attitude… (more)

Subjects/Keywords: Aerospace Engineering; Astrodynamics; Space Vehicles

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APA (6th Edition):

Coulter, N. (2018). Design of an Attitude Control System for a Spacecraft with Propellant Slosh Dynamics. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/424

Chicago Manual of Style (16th Edition):

Coulter, Nolan. “Design of an Attitude Control System for a Spacecraft with Propellant Slosh Dynamics.” 2018. Masters Thesis, Embry-Riddle Aeronautical University. Accessed December 14, 2019. https://commons.erau.edu/edt/424.

MLA Handbook (7th Edition):

Coulter, Nolan. “Design of an Attitude Control System for a Spacecraft with Propellant Slosh Dynamics.” 2018. Web. 14 Dec 2019.

Vancouver:

Coulter N. Design of an Attitude Control System for a Spacecraft with Propellant Slosh Dynamics. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2018. [cited 2019 Dec 14]. Available from: https://commons.erau.edu/edt/424.

Council of Science Editors:

Coulter N. Design of an Attitude Control System for a Spacecraft with Propellant Slosh Dynamics. [Masters Thesis]. Embry-Riddle Aeronautical University; 2018. Available from: https://commons.erau.edu/edt/424


University of Illinois – Urbana-Champaign

8. Ponnapalli, Kaushik. Optimal variable-specific-impulse trajectories in simple gravitational fields.

Degree: MS, Aerospace Engineering, 2019, University of Illinois – Urbana-Champaign

 Minimum-fuel trajectories in the Clohessy-Wiltshire orbital model are investigated. Low-thrust variable-specific-impulse propulsion is assumed. The necessary conditions for an optimal solution and the equations of… (more)

Subjects/Keywords: Astrodynamics, Optimal Trajectories; Trajectory Optimization

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APA (6th Edition):

Ponnapalli, K. (2019). Optimal variable-specific-impulse trajectories in simple gravitational fields. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/104920

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):

Ponnapalli, Kaushik. “Optimal variable-specific-impulse trajectories in simple gravitational fields.” 2019. Thesis, University of Illinois – Urbana-Champaign. Accessed December 14, 2019. http://hdl.handle.net/2142/104920.

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

MLA Handbook (7th Edition):

Ponnapalli, Kaushik. “Optimal variable-specific-impulse trajectories in simple gravitational fields.” 2019. Web. 14 Dec 2019.

Vancouver:

Ponnapalli K. Optimal variable-specific-impulse trajectories in simple gravitational fields. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2019. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/2142/104920.

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

Council of Science Editors:

Ponnapalli K. Optimal variable-specific-impulse trajectories in simple gravitational fields. [Thesis]. University of Illinois – Urbana-Champaign; 2019. Available from: http://hdl.handle.net/2142/104920

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


University of Colorado

9. Geeraert, Jeroen L. Multi-Satellite Orbit Determination Using Interferometric Observables with RF Localization Applications.

Degree: PhD, 2017, University of Colorado

  Very long baseline interferometry (VLBI) specifically same-beam interferometry (SBI), and dual-satellite geolocation are two fields of research not previously connected. This is due to… (more)

Subjects/Keywords: astrodynamics; geolocation; interferometry; orbit determination; Aerospace Engineering

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APA (6th Edition):

Geeraert, J. L. (2017). Multi-Satellite Orbit Determination Using Interferometric Observables with RF Localization Applications. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/192

Chicago Manual of Style (16th Edition):

Geeraert, Jeroen L. “Multi-Satellite Orbit Determination Using Interferometric Observables with RF Localization Applications.” 2017. Doctoral Dissertation, University of Colorado. Accessed December 14, 2019. https://scholar.colorado.edu/asen_gradetds/192.

MLA Handbook (7th Edition):

Geeraert, Jeroen L. “Multi-Satellite Orbit Determination Using Interferometric Observables with RF Localization Applications.” 2017. Web. 14 Dec 2019.

Vancouver:

Geeraert JL. Multi-Satellite Orbit Determination Using Interferometric Observables with RF Localization Applications. [Internet] [Doctoral dissertation]. University of Colorado; 2017. [cited 2019 Dec 14]. Available from: https://scholar.colorado.edu/asen_gradetds/192.

Council of Science Editors:

Geeraert JL. Multi-Satellite Orbit Determination Using Interferometric Observables with RF Localization Applications. [Doctoral Dissertation]. University of Colorado; 2017. Available from: https://scholar.colorado.edu/asen_gradetds/192


Delft University of Technology

10. Hess, J.R. Aerogravity assists: Hypersonic maneuvering to improve planetary gravity assists:.

Degree: 2016, Delft University of Technology

 Interplanetary missions use gravitational slingshots around planetary bodies to adjust their heliocentric velocity or inclination for quite some time. The momentum exchange that can be… (more)

Subjects/Keywords: astrodynamics; aerogravity; gravity; assist; optimization; hypersonics; waverider

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APA (6th Edition):

Hess, J. R. (2016). Aerogravity assists: Hypersonic maneuvering to improve planetary gravity assists:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:dee2d842-ca91-4086-8ef8-771cfee1b0dc

Chicago Manual of Style (16th Edition):

Hess, J R. “Aerogravity assists: Hypersonic maneuvering to improve planetary gravity assists:.” 2016. Masters Thesis, Delft University of Technology. Accessed December 14, 2019. http://resolver.tudelft.nl/uuid:dee2d842-ca91-4086-8ef8-771cfee1b0dc.

MLA Handbook (7th Edition):

Hess, J R. “Aerogravity assists: Hypersonic maneuvering to improve planetary gravity assists:.” 2016. Web. 14 Dec 2019.

Vancouver:

Hess JR. Aerogravity assists: Hypersonic maneuvering to improve planetary gravity assists:. [Internet] [Masters thesis]. Delft University of Technology; 2016. [cited 2019 Dec 14]. Available from: http://resolver.tudelft.nl/uuid:dee2d842-ca91-4086-8ef8-771cfee1b0dc.

Council of Science Editors:

Hess JR. Aerogravity assists: Hypersonic maneuvering to improve planetary gravity assists:. [Masters Thesis]. Delft University of Technology; 2016. Available from: http://resolver.tudelft.nl/uuid:dee2d842-ca91-4086-8ef8-771cfee1b0dc

11. Azari, Pouyan. An Orbit Control System for UWE-4 Using the High Fidelity Simulation Tool Orekit.

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

Cubesats are picosatellites that have a mass of less than 1.3kg and have a shape of acube. As a result of their low cost… (more)

Subjects/Keywords: Orbital mechanics; astrodynamics; small satellites; orbit control

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APA (6th Edition):

Azari, P. (2017). An Orbit Control System for UWE-4 Using the High Fidelity Simulation Tool Orekit. (Thesis). Luleå University of Technology. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-61409

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):

Azari, Pouyan. “An Orbit Control System for UWE-4 Using the High Fidelity Simulation Tool Orekit.” 2017. Thesis, Luleå University of Technology. Accessed December 14, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-61409.

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

MLA Handbook (7th Edition):

Azari, Pouyan. “An Orbit Control System for UWE-4 Using the High Fidelity Simulation Tool Orekit.” 2017. Web. 14 Dec 2019.

Vancouver:

Azari P. An Orbit Control System for UWE-4 Using the High Fidelity Simulation Tool Orekit. [Internet] [Thesis]. Luleå University of Technology; 2017. [cited 2019 Dec 14]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-61409.

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

Council of Science Editors:

Azari P. An Orbit Control System for UWE-4 Using the High Fidelity Simulation Tool Orekit. [Thesis]. Luleå University of Technology; 2017. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-61409

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


University of New South Wales

12. Capon, Christopher. Ionospheric Aerodynamics in Low Earth Orbit.

Degree: Engineering & Information Technology, 2017, University of New South Wales

 Understanding perturbing forces takes on new significance as the Low Earth Orbit (LEO) environment becomes increasingly congested and the risk of collision events that threaten… (more)

Subjects/Keywords: Astrodynamics; Ionospheric Aerodynamics; Space Situational Awareness

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APA (6th Edition):

Capon, C. (2017). Ionospheric Aerodynamics in Low Earth Orbit. (Doctoral Dissertation). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/58652 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:46528/SOURCE01?view=true

Chicago Manual of Style (16th Edition):

Capon, Christopher. “Ionospheric Aerodynamics in Low Earth Orbit.” 2017. Doctoral Dissertation, University of New South Wales. Accessed December 14, 2019. http://handle.unsw.edu.au/1959.4/58652 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:46528/SOURCE01?view=true.

MLA Handbook (7th Edition):

Capon, Christopher. “Ionospheric Aerodynamics in Low Earth Orbit.” 2017. Web. 14 Dec 2019.

Vancouver:

Capon C. Ionospheric Aerodynamics in Low Earth Orbit. [Internet] [Doctoral dissertation]. University of New South Wales; 2017. [cited 2019 Dec 14]. Available from: http://handle.unsw.edu.au/1959.4/58652 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:46528/SOURCE01?view=true.

Council of Science Editors:

Capon C. Ionospheric Aerodynamics in Low Earth Orbit. [Doctoral Dissertation]. University of New South Wales; 2017. Available from: http://handle.unsw.edu.au/1959.4/58652 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:46528/SOURCE01?view=true


Cal Poly

13. Jackson, Daniel J. Formulation of an Optimal Search Strategy for Space Debris At GEO.

Degree: MS, Aerospace Engineering, 2011, Cal Poly

  The purpose of this thesis is to create a search strategy to find orbital debris when the object fails to appear in the sky… (more)

Subjects/Keywords: aerospace; space; debris; GEO; telescope; MODEST; Astrodynamics

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APA (6th Edition):

Jackson, D. J. (2011). Formulation of an Optimal Search Strategy for Space Debris At GEO. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/656 ; 10.15368/theses.2011.202

Chicago Manual of Style (16th Edition):

Jackson, Daniel J. “Formulation of an Optimal Search Strategy for Space Debris At GEO.” 2011. Masters Thesis, Cal Poly. Accessed December 14, 2019. https://digitalcommons.calpoly.edu/theses/656 ; 10.15368/theses.2011.202.

MLA Handbook (7th Edition):

Jackson, Daniel J. “Formulation of an Optimal Search Strategy for Space Debris At GEO.” 2011. Web. 14 Dec 2019.

Vancouver:

Jackson DJ. Formulation of an Optimal Search Strategy for Space Debris At GEO. [Internet] [Masters thesis]. Cal Poly; 2011. [cited 2019 Dec 14]. Available from: https://digitalcommons.calpoly.edu/theses/656 ; 10.15368/theses.2011.202.

Council of Science Editors:

Jackson DJ. Formulation of an Optimal Search Strategy for Space Debris At GEO. [Masters Thesis]. Cal Poly; 2011. Available from: https://digitalcommons.calpoly.edu/theses/656 ; 10.15368/theses.2011.202


Cal Poly

14. Iuliano, Jay R. A Solution to the Circular Restricted N Body Problem in Planetary Systems.

Degree: MS, Aerospace Engineering, 2016, Cal Poly

  This thesis is a brief look at a new solution to a problem that has been approached in many different ways in the past… (more)

Subjects/Keywords: Astrodynamics; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

Iuliano, J. R. (2016). A Solution to the Circular Restricted N Body Problem in Planetary Systems. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1612 ; 10.15368/theses.2016.80

Chicago Manual of Style (16th Edition):

Iuliano, Jay R. “A Solution to the Circular Restricted N Body Problem in Planetary Systems.” 2016. Masters Thesis, Cal Poly. Accessed December 14, 2019. https://digitalcommons.calpoly.edu/theses/1612 ; 10.15368/theses.2016.80.

MLA Handbook (7th Edition):

Iuliano, Jay R. “A Solution to the Circular Restricted N Body Problem in Planetary Systems.” 2016. Web. 14 Dec 2019.

Vancouver:

Iuliano JR. A Solution to the Circular Restricted N Body Problem in Planetary Systems. [Internet] [Masters thesis]. Cal Poly; 2016. [cited 2019 Dec 14]. Available from: https://digitalcommons.calpoly.edu/theses/1612 ; 10.15368/theses.2016.80.

Council of Science Editors:

Iuliano JR. A Solution to the Circular Restricted N Body Problem in Planetary Systems. [Masters Thesis]. Cal Poly; 2016. Available from: https://digitalcommons.calpoly.edu/theses/1612 ; 10.15368/theses.2016.80


Cal Poly

15. Williams, Adrian Michael. Thermal Vacuum Chamber Refurbishment and Analysis.

Degree: MS, Aerospace Engineering, 2018, Cal Poly

  Spacecraft are subject to different environments while on orbit around the Earth and beyond. One of the most critical of these environments that must… (more)

Subjects/Keywords: thermal; vacuum; chamber; space; environments; pressure; Astrodynamics

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APA (6th Edition):

Williams, A. M. (2018). Thermal Vacuum Chamber Refurbishment and Analysis. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1860

Chicago Manual of Style (16th Edition):

Williams, Adrian Michael. “Thermal Vacuum Chamber Refurbishment and Analysis.” 2018. Masters Thesis, Cal Poly. Accessed December 14, 2019. https://digitalcommons.calpoly.edu/theses/1860.

MLA Handbook (7th Edition):

Williams, Adrian Michael. “Thermal Vacuum Chamber Refurbishment and Analysis.” 2018. Web. 14 Dec 2019.

Vancouver:

Williams AM. Thermal Vacuum Chamber Refurbishment and Analysis. [Internet] [Masters thesis]. Cal Poly; 2018. [cited 2019 Dec 14]. Available from: https://digitalcommons.calpoly.edu/theses/1860.

Council of Science Editors:

Williams AM. Thermal Vacuum Chamber Refurbishment and Analysis. [Masters Thesis]. Cal Poly; 2018. Available from: https://digitalcommons.calpoly.edu/theses/1860


University of Colorado

16. McMahon, Jay Warren. An Analytical Theory for the Perturbative Effect of Solar Radiation Pressure on Natural and Artificial Satellites.

Degree: PhD, Aerospace Engineering Sciences, 2011, University of Colorado

  Solar radiation pressure is the largest non-gravitational perturbation for most satellites in the solar system, and can therefore have a significant influence on their… (more)

Subjects/Keywords: astrodynamics; BYORP; celestial mechanics; orbital dynamics; orbit determination; solar radiation pressure; Aerospace Engineering; Astrodynamics

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APA (6th Edition):

McMahon, J. W. (2011). An Analytical Theory for the Perturbative Effect of Solar Radiation Pressure on Natural and Artificial Satellites. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/26

Chicago Manual of Style (16th Edition):

McMahon, Jay Warren. “An Analytical Theory for the Perturbative Effect of Solar Radiation Pressure on Natural and Artificial Satellites.” 2011. Doctoral Dissertation, University of Colorado. Accessed December 14, 2019. https://scholar.colorado.edu/asen_gradetds/26.

MLA Handbook (7th Edition):

McMahon, Jay Warren. “An Analytical Theory for the Perturbative Effect of Solar Radiation Pressure on Natural and Artificial Satellites.” 2011. Web. 14 Dec 2019.

Vancouver:

McMahon JW. An Analytical Theory for the Perturbative Effect of Solar Radiation Pressure on Natural and Artificial Satellites. [Internet] [Doctoral dissertation]. University of Colorado; 2011. [cited 2019 Dec 14]. Available from: https://scholar.colorado.edu/asen_gradetds/26.

Council of Science Editors:

McMahon JW. An Analytical Theory for the Perturbative Effect of Solar Radiation Pressure on Natural and Artificial Satellites. [Doctoral Dissertation]. University of Colorado; 2011. Available from: https://scholar.colorado.edu/asen_gradetds/26


University of Colorado

17. De Smet, Stijn. On the Design of Solar Gravity Driven Planetocentric Transfers Using Artificial Neural Networks.

Degree: PhD, 2018, University of Colorado

  The sun's gravity can be used to efficiently transfer between different planetocentric orbits. Such transfers cannot be designed in a two-body dynamical system, nor… (more)

Subjects/Keywords: artificial neural networks; astrodynamics; eccentric hill system; machine learning; periapse poincaré maps; Aerospace Engineering; Astrodynamics; Computer Sciences

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APA (6th Edition):

De Smet, S. (2018). On the Design of Solar Gravity Driven Planetocentric Transfers Using Artificial Neural Networks. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/235

Chicago Manual of Style (16th Edition):

De Smet, Stijn. “On the Design of Solar Gravity Driven Planetocentric Transfers Using Artificial Neural Networks.” 2018. Doctoral Dissertation, University of Colorado. Accessed December 14, 2019. https://scholar.colorado.edu/asen_gradetds/235.

MLA Handbook (7th Edition):

De Smet, Stijn. “On the Design of Solar Gravity Driven Planetocentric Transfers Using Artificial Neural Networks.” 2018. Web. 14 Dec 2019.

Vancouver:

De Smet S. On the Design of Solar Gravity Driven Planetocentric Transfers Using Artificial Neural Networks. [Internet] [Doctoral dissertation]. University of Colorado; 2018. [cited 2019 Dec 14]. Available from: https://scholar.colorado.edu/asen_gradetds/235.

Council of Science Editors:

De Smet S. On the Design of Solar Gravity Driven Planetocentric Transfers Using Artificial Neural Networks. [Doctoral Dissertation]. University of Colorado; 2018. Available from: https://scholar.colorado.edu/asen_gradetds/235


University of Colorado

18. Baresi, Nicola. Spacecraft Formation Flight on Quasi-Periodic Invariant Tori.

Degree: PhD, 2017, University of Colorado

  Since the successful rendezvous of the Gemini VI and VII spacecraft in 1965, spacecraft formation flying has attracted the interest of many researchers in… (more)

Subjects/Keywords: astrodynamics; cluster flight; dynamical systems theory; quasi-periodic invariant tori; spacecraft formation flying; Aerospace Engineering; Astrodynamics

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APA (6th Edition):

Baresi, N. (2017). Spacecraft Formation Flight on Quasi-Periodic Invariant Tori. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/219

Chicago Manual of Style (16th Edition):

Baresi, Nicola. “Spacecraft Formation Flight on Quasi-Periodic Invariant Tori.” 2017. Doctoral Dissertation, University of Colorado. Accessed December 14, 2019. https://scholar.colorado.edu/asen_gradetds/219.

MLA Handbook (7th Edition):

Baresi, Nicola. “Spacecraft Formation Flight on Quasi-Periodic Invariant Tori.” 2017. Web. 14 Dec 2019.

Vancouver:

Baresi N. Spacecraft Formation Flight on Quasi-Periodic Invariant Tori. [Internet] [Doctoral dissertation]. University of Colorado; 2017. [cited 2019 Dec 14]. Available from: https://scholar.colorado.edu/asen_gradetds/219.

Council of Science Editors:

Baresi N. Spacecraft Formation Flight on Quasi-Periodic Invariant Tori. [Doctoral Dissertation]. University of Colorado; 2017. Available from: https://scholar.colorado.edu/asen_gradetds/219


The Ohio State University

19. Poli, C. A study of the effect of man's motion on the attitude and orbital motion of a satellite.

Degree: PhD, Graduate School, 1965, The Ohio State University

Subjects/Keywords: Education; Artificial satellites; Astrodynamics

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APA (6th Edition):

Poli, C. (1965). A study of the effect of man's motion on the attitude and orbital motion of a satellite. (Doctoral Dissertation). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1486567958464808

Chicago Manual of Style (16th Edition):

Poli, C. “A study of the effect of man's motion on the attitude and orbital motion of a satellite.” 1965. Doctoral Dissertation, The Ohio State University. Accessed December 14, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=osu1486567958464808.

MLA Handbook (7th Edition):

Poli, C. “A study of the effect of man's motion on the attitude and orbital motion of a satellite.” 1965. Web. 14 Dec 2019.

Vancouver:

Poli C. A study of the effect of man's motion on the attitude and orbital motion of a satellite. [Internet] [Doctoral dissertation]. The Ohio State University; 1965. [cited 2019 Dec 14]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1486567958464808.

Council of Science Editors:

Poli C. A study of the effect of man's motion on the attitude and orbital motion of a satellite. [Doctoral Dissertation]. The Ohio State University; 1965. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1486567958464808


Texas A&M University

20. Johnson, Kirk Wayne. Approaches for Modeling Satellite Relative Motion.

Degree: 2016, Texas A&M University

 This dissertation explores new approaches for modeling perturbed and unperturbed satellite relative motion. It extends Hoots orbit theory, an analytical averaging-method perturbation solution to the… (more)

Subjects/Keywords: Satellite Relative Motion; Satellite Formation Flying; Zonal Problem; Astrodynamics

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APA (6th Edition):

Johnson, K. W. (2016). Approaches for Modeling Satellite Relative Motion. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/158945

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):

Johnson, Kirk Wayne. “Approaches for Modeling Satellite Relative Motion.” 2016. Thesis, Texas A&M University. Accessed December 14, 2019. http://hdl.handle.net/1969.1/158945.

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

MLA Handbook (7th Edition):

Johnson, Kirk Wayne. “Approaches for Modeling Satellite Relative Motion.” 2016. Web. 14 Dec 2019.

Vancouver:

Johnson KW. Approaches for Modeling Satellite Relative Motion. [Internet] [Thesis]. Texas A&M University; 2016. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/1969.1/158945.

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

Council of Science Editors:

Johnson KW. Approaches for Modeling Satellite Relative Motion. [Thesis]. Texas A&M University; 2016. Available from: http://hdl.handle.net/1969.1/158945

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


Penn State University

21. Reiter, Jason A. Numerical And Analytical Solutions To Rapid Collision Avoidance Maneuvers Constrained By Mission Performance Requirements.

Degree: MS, Aerospace Engineering, 2016, Penn State University

 Collision avoidance maneuvers to prevent orbital collisions between two catalogued objects are typically planned multiple days in advance. If the warning time is decreased to… (more)

Subjects/Keywords: astrodynamics; collision avoidance; debris; trade studies; optimization; trajectory; mission design

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APA (6th Edition):

Reiter, J. A. (2016). Numerical And Analytical Solutions To Rapid Collision Avoidance Maneuvers Constrained By Mission Performance Requirements. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/29469

Chicago Manual of Style (16th Edition):

Reiter, Jason A. “Numerical And Analytical Solutions To Rapid Collision Avoidance Maneuvers Constrained By Mission Performance Requirements.” 2016. Masters Thesis, Penn State University. Accessed December 14, 2019. https://etda.libraries.psu.edu/catalog/29469.

MLA Handbook (7th Edition):

Reiter, Jason A. “Numerical And Analytical Solutions To Rapid Collision Avoidance Maneuvers Constrained By Mission Performance Requirements.” 2016. Web. 14 Dec 2019.

Vancouver:

Reiter JA. Numerical And Analytical Solutions To Rapid Collision Avoidance Maneuvers Constrained By Mission Performance Requirements. [Internet] [Masters thesis]. Penn State University; 2016. [cited 2019 Dec 14]. Available from: https://etda.libraries.psu.edu/catalog/29469.

Council of Science Editors:

Reiter JA. Numerical And Analytical Solutions To Rapid Collision Avoidance Maneuvers Constrained By Mission Performance Requirements. [Masters Thesis]. Penn State University; 2016. Available from: https://etda.libraries.psu.edu/catalog/29469


Penn State University

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

Degree: PhD, Aerospace Engineering, 2010, Penn State University

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Scott, Christopher James. “Transfer and Capture into Distant Retrograde Orbits.” 2010. Doctoral Dissertation, Penn State University. Accessed December 14, 2019. https://etda.libraries.psu.edu/catalog/10471.

MLA Handbook (7th Edition):

Scott, Christopher James. “Transfer and Capture into Distant Retrograde Orbits.” 2010. Web. 14 Dec 2019.

Vancouver:

Scott CJ. Transfer and Capture into Distant Retrograde Orbits. [Internet] [Doctoral dissertation]. Penn State University; 2010. [cited 2019 Dec 14]. Available from: https://etda.libraries.psu.edu/catalog/10471.

Council of Science Editors:

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


Penn State University

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

Degree: MS, Aerospace Engineering, 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. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/29463

Chicago Manual of Style (16th Edition):

Kuppa, Koundinya. “Long-term Orbit Propagation Using Symplectic Integration Algorithms.” 2016. Masters Thesis, Penn State University. Accessed December 14, 2019. https://etda.libraries.psu.edu/catalog/29463.

MLA Handbook (7th Edition):

Kuppa, Koundinya. “Long-term Orbit Propagation Using Symplectic Integration Algorithms.” 2016. Web. 14 Dec 2019.

Vancouver:

Kuppa K. Long-term Orbit Propagation Using Symplectic Integration Algorithms. [Internet] [Masters thesis]. Penn State University; 2016. [cited 2019 Dec 14]. Available from: https://etda.libraries.psu.edu/catalog/29463.

Council of Science Editors:

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


Penn State University

24. Sottile, Bradley Joseph. Evolutionary Computation for Spacecraft Trajectory Optimization.

Degree: MS, Aerospace Engineering, 2013, Penn State University

 Evolutionary Computation has exploded in use in engineering and the applied sciences. For this thesis, three algorithms – Particle Swarm Optimization (PSO), Bacteria Foraging Optimization… (more)

Subjects/Keywords: Astrodynamics; Evolutionary Algorithms; Evolutionary Computation; Evolutionary Strategies; Optimization; Spacecraft Trajectory

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APA (6th Edition):

Sottile, B. J. (2013). Evolutionary Computation for Spacecraft Trajectory Optimization. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/19135

Chicago Manual of Style (16th Edition):

Sottile, Bradley Joseph. “Evolutionary Computation for Spacecraft Trajectory Optimization.” 2013. Masters Thesis, Penn State University. Accessed December 14, 2019. https://etda.libraries.psu.edu/catalog/19135.

MLA Handbook (7th Edition):

Sottile, Bradley Joseph. “Evolutionary Computation for Spacecraft Trajectory Optimization.” 2013. Web. 14 Dec 2019.

Vancouver:

Sottile BJ. Evolutionary Computation for Spacecraft Trajectory Optimization. [Internet] [Masters thesis]. Penn State University; 2013. [cited 2019 Dec 14]. Available from: https://etda.libraries.psu.edu/catalog/19135.

Council of Science Editors:

Sottile BJ. Evolutionary Computation for Spacecraft Trajectory Optimization. [Masters Thesis]. Penn State University; 2013. Available from: https://etda.libraries.psu.edu/catalog/19135


University of Southern California

25. Sarzi Amade', Nicola. Mars rapid round trip mission design.

Degree: PhD, Astronautical Engineering, 2010, University of Southern California

 The present research is divided in two parts. The first part is a well defined mathematical problem, with exact rules and results, in which the… (more)

Subjects/Keywords: Mars; astrodynamics; roundtrip; rapid roundtrip; human spaceflight; systems engineering; mission design

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APA (6th Edition):

Sarzi Amade', N. (2010). Mars rapid round trip mission design. (Doctoral Dissertation). University of Southern California. Retrieved from http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll127/id/361721/rec/3962

Chicago Manual of Style (16th Edition):

Sarzi Amade', Nicola. “Mars rapid round trip mission design.” 2010. Doctoral Dissertation, University of Southern California. Accessed December 14, 2019. http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll127/id/361721/rec/3962.

MLA Handbook (7th Edition):

Sarzi Amade', Nicola. “Mars rapid round trip mission design.” 2010. Web. 14 Dec 2019.

Vancouver:

Sarzi Amade' N. Mars rapid round trip mission design. [Internet] [Doctoral dissertation]. University of Southern California; 2010. [cited 2019 Dec 14]. Available from: http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll127/id/361721/rec/3962.

Council of Science Editors:

Sarzi Amade' N. Mars rapid round trip mission design. [Doctoral Dissertation]. University of Southern California; 2010. Available from: http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll127/id/361721/rec/3962

26. Conte, Davide. Determination of Optimal Earth-mars Trajectories to Target the Moons of Mars.

Degree: MS, Aerospace Engineering, 2014, Penn State University

 The focus of this thesis is to analyze interplanetary transfer maneuvers from Earth to Mars in order to target the Martian moons, Phobos and Deimos.… (more)

Subjects/Keywords: Mars; Phobos; Deimos; astrodynamics

…undergraduate and graduate theses, and especially for teaching Interplanetary Astrodynamics, one of… …in the field of astrodynamics that the Swiss mathematician Johann Heinrich Lambert… …astrodynamics, Lambert’s problem is a two-point boundary value problem (see Figure 8) for… …eccentricity. Such derivation can be found in most astrodynamics textbooks such as Prussing and… 

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APA (6th Edition):

Conte, D. (2014). Determination of Optimal Earth-mars Trajectories to Target the Moons of Mars. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/21382

Chicago Manual of Style (16th Edition):

Conte, Davide. “Determination of Optimal Earth-mars Trajectories to Target the Moons of Mars.” 2014. Masters Thesis, Penn State University. Accessed December 14, 2019. https://etda.libraries.psu.edu/catalog/21382.

MLA Handbook (7th Edition):

Conte, Davide. “Determination of Optimal Earth-mars Trajectories to Target the Moons of Mars.” 2014. Web. 14 Dec 2019.

Vancouver:

Conte D. Determination of Optimal Earth-mars Trajectories to Target the Moons of Mars. [Internet] [Masters thesis]. Penn State University; 2014. [cited 2019 Dec 14]. Available from: https://etda.libraries.psu.edu/catalog/21382.

Council of Science Editors:

Conte D. Determination of Optimal Earth-mars Trajectories to Target the Moons of Mars. [Masters Thesis]. Penn State University; 2014. Available from: https://etda.libraries.psu.edu/catalog/21382


Virginia Tech

27. Rogers, Andrew Charles. Optimization-Based Guidance for Satellite Relative Motion.

Degree: PhD, Aerospace and Ocean Engineering, 2016, Virginia Tech

 Spacecraft relative motion modeling and control promises to enable or augment a wide range of missions for scientific research, military applications, and space situational awareness.… (more)

Subjects/Keywords: Model predictive control; astrodynamics; optimal control; optimization; proximity operations

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APA (6th Edition):

Rogers, A. C. (2016). Optimization-Based Guidance for Satellite Relative Motion. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/79455

Chicago Manual of Style (16th Edition):

Rogers, Andrew Charles. “Optimization-Based Guidance for Satellite Relative Motion.” 2016. Doctoral Dissertation, Virginia Tech. Accessed December 14, 2019. http://hdl.handle.net/10919/79455.

MLA Handbook (7th Edition):

Rogers, Andrew Charles. “Optimization-Based Guidance for Satellite Relative Motion.” 2016. Web. 14 Dec 2019.

Vancouver:

Rogers AC. Optimization-Based Guidance for Satellite Relative Motion. [Internet] [Doctoral dissertation]. Virginia Tech; 2016. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/10919/79455.

Council of Science Editors:

Rogers AC. Optimization-Based Guidance for Satellite Relative Motion. [Doctoral Dissertation]. Virginia Tech; 2016. Available from: http://hdl.handle.net/10919/79455

28. Polzine, Benjamin. The Collisional Evolution of Orbital Debris in Geopotential Wells and Disposal Orbits.

Degree: MS, Aerospace Engineering, 2017, Cal Poly

  This thesis investigates the orbital debris evolution in the geosynchronous disposal orbit regime and within geosynchronous orbits effected by the geopotential wells. A propagator… (more)

Subjects/Keywords: Breakup; Perturbation; Debris; Astrodynamics

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APA (6th Edition):

Polzine, B. (2017). The Collisional Evolution of Orbital Debris in Geopotential Wells and Disposal Orbits. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1703

Chicago Manual of Style (16th Edition):

Polzine, Benjamin. “The Collisional Evolution of Orbital Debris in Geopotential Wells and Disposal Orbits.” 2017. Masters Thesis, Cal Poly. Accessed December 14, 2019. https://digitalcommons.calpoly.edu/theses/1703.

MLA Handbook (7th Edition):

Polzine, Benjamin. “The Collisional Evolution of Orbital Debris in Geopotential Wells and Disposal Orbits.” 2017. Web. 14 Dec 2019.

Vancouver:

Polzine B. The Collisional Evolution of Orbital Debris in Geopotential Wells and Disposal Orbits. [Internet] [Masters thesis]. Cal Poly; 2017. [cited 2019 Dec 14]. Available from: https://digitalcommons.calpoly.edu/theses/1703.

Council of Science Editors:

Polzine B. The Collisional Evolution of Orbital Debris in Geopotential Wells and Disposal Orbits. [Masters Thesis]. Cal Poly; 2017. Available from: https://digitalcommons.calpoly.edu/theses/1703

29. Avendaño González, Martín Eugenio. Flower Constellations: Optimization and Applications.

Degree: 2013, Universidad de Zaragoza, Prensas de la Universidad

 Un satélite artificial es un objeto diseñado por el ser humano y lanzado al espacio mediante un vehículo espacial con el objetivo de sobrellevar una… (more)

Subjects/Keywords: astrodinámica; constelaciones de satélites; optimización; astrodynamics; satellite constellations; optimization

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APA (6th Edition):

Avendaño González, M. E. (2013). Flower Constellations: Optimization and Applications. (Thesis). Universidad de Zaragoza, Prensas de la Universidad. Retrieved from http://zaguan.unizar.es/record/11733

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):

Avendaño González, Martín Eugenio. “Flower Constellations: Optimization and Applications.” 2013. Thesis, Universidad de Zaragoza, Prensas de la Universidad. Accessed December 14, 2019. http://zaguan.unizar.es/record/11733.

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

MLA Handbook (7th Edition):

Avendaño González, Martín Eugenio. “Flower Constellations: Optimization and Applications.” 2013. Web. 14 Dec 2019.

Vancouver:

Avendaño González ME. Flower Constellations: Optimization and Applications. [Internet] [Thesis]. Universidad de Zaragoza, Prensas de la Universidad; 2013. [cited 2019 Dec 14]. Available from: http://zaguan.unizar.es/record/11733.

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

Council of Science Editors:

Avendaño González ME. Flower Constellations: Optimization and Applications. [Thesis]. Universidad de Zaragoza, Prensas de la Universidad; 2013. Available from: http://zaguan.unizar.es/record/11733

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


Delft University of Technology

30. Hoogland, J. Earth frozen orbits: design, injection and stability:.

Degree: 2016, Delft University of Technology

 A frozen orbit is an orbit chosen such that the effect of perturbations on (a combination of) the mean orbital elements is minimized. The concept… (more)

Subjects/Keywords: astrodynamics; frozen orbit; orbital perturbations; mission design; optimization; orbit injection

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APA (6th Edition):

Hoogland, J. (2016). Earth frozen orbits: design, injection and stability:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:fc0a57ce-33df-4cd2-a61b-66e702cc9cf8

Chicago Manual of Style (16th Edition):

Hoogland, J. “Earth frozen orbits: design, injection and stability:.” 2016. Masters Thesis, Delft University of Technology. Accessed December 14, 2019. http://resolver.tudelft.nl/uuid:fc0a57ce-33df-4cd2-a61b-66e702cc9cf8.

MLA Handbook (7th Edition):

Hoogland, J. “Earth frozen orbits: design, injection and stability:.” 2016. Web. 14 Dec 2019.

Vancouver:

Hoogland J. Earth frozen orbits: design, injection and stability:. [Internet] [Masters thesis]. Delft University of Technology; 2016. [cited 2019 Dec 14]. Available from: http://resolver.tudelft.nl/uuid:fc0a57ce-33df-4cd2-a61b-66e702cc9cf8.

Council of Science Editors:

Hoogland J. Earth frozen orbits: design, injection and stability:. [Masters Thesis]. Delft University of Technology; 2016. Available from: http://resolver.tudelft.nl/uuid:fc0a57ce-33df-4cd2-a61b-66e702cc9cf8

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