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You searched for subject:(Orbital Mechanics). Showing records 1 – 30 of 52 total matches.

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Penn State University

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

Degree: 2016, Penn State University

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

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

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APA (6th Edition):

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

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

Chicago Manual of Style (16th Edition):

Kuppa, Koundinya. “Long-term Orbit Propagation Using Symplectic Integration Algorithms.” 2016. Thesis, Penn State University. Accessed January 21, 2021. https://submit-etda.libraries.psu.edu/catalog/29463.

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

MLA Handbook (7th Edition):

Kuppa, Koundinya. “Long-term Orbit Propagation Using Symplectic Integration Algorithms.” 2016. Web. 21 Jan 2021.

Vancouver:

Kuppa K. Long-term Orbit Propagation Using Symplectic Integration Algorithms. [Internet] [Thesis]. Penn State University; 2016. [cited 2021 Jan 21]. Available from: https://submit-etda.libraries.psu.edu/catalog/29463.

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

Council of Science Editors:

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

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


University of Arizona

2. Burnett, Ethan Ryan. Relative Orbital Motion Dynamical Models for Orbits about Nonspherical Bodies .

Degree: 2018, University of Arizona

 Relative orbital motion dynamical models are presented and discussed. Two types of models are primarily discussed in this work: a linear relative motion model accounting… (more)

Subjects/Keywords: aerospace; asteroids; astrodynamics; celestial mechanics; orbital mechanics; spacecraft

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APA (6th Edition):

Burnett, E. R. (2018). Relative Orbital Motion Dynamical Models for Orbits about Nonspherical Bodies . (Masters Thesis). University of Arizona. Retrieved from http://hdl.handle.net/10150/628098

Chicago Manual of Style (16th Edition):

Burnett, Ethan Ryan. “Relative Orbital Motion Dynamical Models for Orbits about Nonspherical Bodies .” 2018. Masters Thesis, University of Arizona. Accessed January 21, 2021. http://hdl.handle.net/10150/628098.

MLA Handbook (7th Edition):

Burnett, Ethan Ryan. “Relative Orbital Motion Dynamical Models for Orbits about Nonspherical Bodies .” 2018. Web. 21 Jan 2021.

Vancouver:

Burnett ER. Relative Orbital Motion Dynamical Models for Orbits about Nonspherical Bodies . [Internet] [Masters thesis]. University of Arizona; 2018. [cited 2021 Jan 21]. Available from: http://hdl.handle.net/10150/628098.

Council of Science Editors:

Burnett ER. Relative Orbital Motion Dynamical Models for Orbits about Nonspherical Bodies . [Masters Thesis]. University of Arizona; 2018. Available from: http://hdl.handle.net/10150/628098


Rochester Institute of Technology

3. Dubill, Amber. Attitude Control for Circumnavigating the Sun with Diffractive Solar Sails.

Degree: MS, Mechanical Engineering, 2020, Rochester Institute of Technology

  A solar sail making use of the physics of diffracted light enables the transfer of optical to mechanical momentum for in-space propulsion. In this… (more)

Subjects/Keywords: Attitude control; Diffractice; Heliophysics; Orbital mechanics; Solar sailing; Spacecraft

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APA (6th Edition):

Dubill, A. (2020). Attitude Control for Circumnavigating the Sun with Diffractive Solar Sails. (Masters Thesis). Rochester Institute of Technology. Retrieved from https://scholarworks.rit.edu/theses/10388

Chicago Manual of Style (16th Edition):

Dubill, Amber. “Attitude Control for Circumnavigating the Sun with Diffractive Solar Sails.” 2020. Masters Thesis, Rochester Institute of Technology. Accessed January 21, 2021. https://scholarworks.rit.edu/theses/10388.

MLA Handbook (7th Edition):

Dubill, Amber. “Attitude Control for Circumnavigating the Sun with Diffractive Solar Sails.” 2020. Web. 21 Jan 2021.

Vancouver:

Dubill A. Attitude Control for Circumnavigating the Sun with Diffractive Solar Sails. [Internet] [Masters thesis]. Rochester Institute of Technology; 2020. [cited 2021 Jan 21]. Available from: https://scholarworks.rit.edu/theses/10388.

Council of Science Editors:

Dubill A. Attitude Control for Circumnavigating the Sun with Diffractive Solar Sails. [Masters Thesis]. Rochester Institute of Technology; 2020. Available from: https://scholarworks.rit.edu/theses/10388


Delft University of Technology

4. Gondelach, D. (author). A Hodographic-Shaping Method for Low-Thrust Trajectory Design.

Degree: 2012, Delft University of Technology

 The goal of this research was to develop an analytic low-thrust trajectory design method. The term low thrust stems form the fact that current electric… (more)

Subjects/Keywords: shape-based method; low-thrust transfer; orbital mechanics

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APA (6th Edition):

Gondelach, D. (. (2012). A Hodographic-Shaping Method for Low-Thrust Trajectory Design. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:6a4f1673-88b1-4823-b2ef-9d864c84ab11

Chicago Manual of Style (16th Edition):

Gondelach, D (author). “A Hodographic-Shaping Method for Low-Thrust Trajectory Design.” 2012. Masters Thesis, Delft University of Technology. Accessed January 21, 2021. http://resolver.tudelft.nl/uuid:6a4f1673-88b1-4823-b2ef-9d864c84ab11.

MLA Handbook (7th Edition):

Gondelach, D (author). “A Hodographic-Shaping Method for Low-Thrust Trajectory Design.” 2012. Web. 21 Jan 2021.

Vancouver:

Gondelach D(. A Hodographic-Shaping Method for Low-Thrust Trajectory Design. [Internet] [Masters thesis]. Delft University of Technology; 2012. [cited 2021 Jan 21]. Available from: http://resolver.tudelft.nl/uuid:6a4f1673-88b1-4823-b2ef-9d864c84ab11.

Council of Science Editors:

Gondelach D(. A Hodographic-Shaping Method for Low-Thrust Trajectory Design. [Masters Thesis]. Delft University of Technology; 2012. Available from: http://resolver.tudelft.nl/uuid:6a4f1673-88b1-4823-b2ef-9d864c84ab11


University of Minnesota

5. Chandramouli, Harini. Effects of a Rogue Star on Earth's Climate.

Degree: PhD, Mathematics, 2020, University of Minnesota

 The details of the way in which the Earth orbits the Sun can have profound effects on Earth’s climate. Elements such as the Earth’s tilt… (more)

Subjects/Keywords: Celestial mechanics; Dynamical systems; Geological record; Milankovitch cycles; Orbital elements

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APA (6th Edition):

Chandramouli, H. (2020). Effects of a Rogue Star on Earth's Climate. (Doctoral Dissertation). University of Minnesota. Retrieved from http://hdl.handle.net/11299/216900

Chicago Manual of Style (16th Edition):

Chandramouli, Harini. “Effects of a Rogue Star on Earth's Climate.” 2020. Doctoral Dissertation, University of Minnesota. Accessed January 21, 2021. http://hdl.handle.net/11299/216900.

MLA Handbook (7th Edition):

Chandramouli, Harini. “Effects of a Rogue Star on Earth's Climate.” 2020. Web. 21 Jan 2021.

Vancouver:

Chandramouli H. Effects of a Rogue Star on Earth's Climate. [Internet] [Doctoral dissertation]. University of Minnesota; 2020. [cited 2021 Jan 21]. Available from: http://hdl.handle.net/11299/216900.

Council of Science Editors:

Chandramouli H. Effects of a Rogue Star on Earth's Climate. [Doctoral Dissertation]. University of Minnesota; 2020. Available from: http://hdl.handle.net/11299/216900


Virginia Tech

6. Ojeda Romero, Juan Andre. Dual Satellite Coverage using Particle Swarm Optimization.

Degree: MS, Aerospace Engineering, 2014, Virginia Tech

 A dual satellite system in a Low Earth Orbit, LEO, would be beneficial to study the electromagnetic occurrences in the magnetosphere and their contributions to… (more)

Subjects/Keywords: particle swarm optimization; space weather; aurora borealis; orbital mechanics; satellite coverage

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APA (6th Edition):

Ojeda Romero, J. A. (2014). Dual Satellite Coverage using Particle Swarm Optimization. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/50627

Chicago Manual of Style (16th Edition):

Ojeda Romero, Juan Andre. “Dual Satellite Coverage using Particle Swarm Optimization.” 2014. Masters Thesis, Virginia Tech. Accessed January 21, 2021. http://hdl.handle.net/10919/50627.

MLA Handbook (7th Edition):

Ojeda Romero, Juan Andre. “Dual Satellite Coverage using Particle Swarm Optimization.” 2014. Web. 21 Jan 2021.

Vancouver:

Ojeda Romero JA. Dual Satellite Coverage using Particle Swarm Optimization. [Internet] [Masters thesis]. Virginia Tech; 2014. [cited 2021 Jan 21]. Available from: http://hdl.handle.net/10919/50627.

Council of Science Editors:

Ojeda Romero JA. Dual Satellite Coverage using Particle Swarm Optimization. [Masters Thesis]. Virginia Tech; 2014. Available from: http://hdl.handle.net/10919/50627


University of Illinois – Urbana-Champaign

7. De La Mata, Jorge. Optimal strategies for selecting from multiple asteroid interception targets.

Degree: MS, 4048, 2014, University of Illinois – Urbana-Champaign

 The goal of this thesis is to demonstrate the applicability of the discrimination time optimization problem to space systems. The concept is applied to an… (more)

Subjects/Keywords: Astrodynamics; Orbital Mechanics; Optimization; Nonlinear Programming; Space; Aerospace; Optimal trajectories; Controls

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APA (6th Edition):

De La Mata, J. (2014). Optimal strategies for selecting from multiple asteroid interception targets. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/50647

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):

De La Mata, Jorge. “Optimal strategies for selecting from multiple asteroid interception targets.” 2014. Thesis, University of Illinois – Urbana-Champaign. Accessed January 21, 2021. http://hdl.handle.net/2142/50647.

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

MLA Handbook (7th Edition):

De La Mata, Jorge. “Optimal strategies for selecting from multiple asteroid interception targets.” 2014. Web. 21 Jan 2021.

Vancouver:

De La Mata J. Optimal strategies for selecting from multiple asteroid interception targets. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2014. [cited 2021 Jan 21]. Available from: http://hdl.handle.net/2142/50647.

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

Council of Science Editors:

De La Mata J. Optimal strategies for selecting from multiple asteroid interception targets. [Thesis]. University of Illinois – Urbana-Champaign; 2014. Available from: http://hdl.handle.net/2142/50647

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


Virginia Tech

8. Karlgaard, Christopher David. Second-Order Relative Motion Equations.

Degree: MS, Aerospace and Ocean Engineering, 2001, Virginia Tech

 This thesis presents an approximate solution of second order relative motion equations. The equations of motion for a Keplerian orbit in spherical coordinates are expanded… (more)

Subjects/Keywords: Orbital Mechanics; Perturbation Methods

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APA (6th Edition):

Karlgaard, C. D. (2001). Second-Order Relative Motion Equations. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/34025

Chicago Manual of Style (16th Edition):

Karlgaard, Christopher David. “Second-Order Relative Motion Equations.” 2001. Masters Thesis, Virginia Tech. Accessed January 21, 2021. http://hdl.handle.net/10919/34025.

MLA Handbook (7th Edition):

Karlgaard, Christopher David. “Second-Order Relative Motion Equations.” 2001. Web. 21 Jan 2021.

Vancouver:

Karlgaard CD. Second-Order Relative Motion Equations. [Internet] [Masters thesis]. Virginia Tech; 2001. [cited 2021 Jan 21]. Available from: http://hdl.handle.net/10919/34025.

Council of Science Editors:

Karlgaard CD. Second-Order Relative Motion Equations. [Masters Thesis]. Virginia Tech; 2001. Available from: http://hdl.handle.net/10919/34025


University of Texas – Austin

9. Pasupathy, Muthukumar. A comparison of range and range-rate based GRACE gravity field solutions.

Degree: MSin Engineering, Aerospace Engineering, 2011, University of Texas – Austin

 In the generation of the standard GRACE gravity fields, the K-Band Ranging (KBR) system data is used in its range-rate mode. Because time derivatives attenuate… (more)

Subjects/Keywords: GRACE mission; Range-Rate; Gravitational fields; Orbital mechanics; Earth gravity

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APA (6th Edition):

Pasupathy, M. (2011). A comparison of range and range-rate based GRACE gravity field solutions. (Masters Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/ETD-UT-2011-05-2818

Chicago Manual of Style (16th Edition):

Pasupathy, Muthukumar. “A comparison of range and range-rate based GRACE gravity field solutions.” 2011. Masters Thesis, University of Texas – Austin. Accessed January 21, 2021. http://hdl.handle.net/2152/ETD-UT-2011-05-2818.

MLA Handbook (7th Edition):

Pasupathy, Muthukumar. “A comparison of range and range-rate based GRACE gravity field solutions.” 2011. Web. 21 Jan 2021.

Vancouver:

Pasupathy M. A comparison of range and range-rate based GRACE gravity field solutions. [Internet] [Masters thesis]. University of Texas – Austin; 2011. [cited 2021 Jan 21]. Available from: http://hdl.handle.net/2152/ETD-UT-2011-05-2818.

Council of Science Editors:

Pasupathy M. A comparison of range and range-rate based GRACE gravity field solutions. [Masters Thesis]. University of Texas – Austin; 2011. Available from: http://hdl.handle.net/2152/ETD-UT-2011-05-2818


Ryerson University

10. Frias, Alexander. Modeling And Control Of Spacecraft Systems With Coupled Orbital And Attitude Dynamics.

Degree: 2012, Ryerson University

 Spacecraft formation flying with coupled orbital-attitude dynamics is one of the most intriguing topics in the field of astronautics. Orbital-attitude coupling is induced when a… (more)

Subjects/Keywords: Space vehicles  – Design and construction; Astronautics  – Systems engineering; Orbital mechanics; Space vehicles  – Control systems

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APA (6th Edition):

Frias, A. (2012). Modeling And Control Of Spacecraft Systems With Coupled Orbital And Attitude Dynamics. (Thesis). Ryerson University. Retrieved from https://digital.library.ryerson.ca/islandora/object/RULA%3A1610

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):

Frias, Alexander. “Modeling And Control Of Spacecraft Systems With Coupled Orbital And Attitude Dynamics.” 2012. Thesis, Ryerson University. Accessed January 21, 2021. https://digital.library.ryerson.ca/islandora/object/RULA%3A1610.

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

MLA Handbook (7th Edition):

Frias, Alexander. “Modeling And Control Of Spacecraft Systems With Coupled Orbital And Attitude Dynamics.” 2012. Web. 21 Jan 2021.

Vancouver:

Frias A. Modeling And Control Of Spacecraft Systems With Coupled Orbital And Attitude Dynamics. [Internet] [Thesis]. Ryerson University; 2012. [cited 2021 Jan 21]. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A1610.

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

Council of Science Editors:

Frias A. Modeling And Control Of Spacecraft Systems With Coupled Orbital And Attitude Dynamics. [Thesis]. Ryerson University; 2012. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A1610

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


University of Colorado

11. 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 January 21, 2021. 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. 21 Jan 2021.

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 2021 Jan 21]. 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

12. 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; Aerospace Engineering; Rymd- och flygteknik

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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 January 21, 2021. 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. 21 Jan 2021.

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 2021 Jan 21]. 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


Iowa State University

13. Wagner, Samuel Arthur. Automated trajectory design for impulsive and low thrust interplanetary mission analysis.

Degree: 2014, Iowa State University

 This dissertation describes a hybrid optimization algorithm that is able to determine optimal trajectories for many complex mission analysis and design orbital mechanics problems. This… (more)

Subjects/Keywords: Aerospace Engineering; Astrodynamics; Genetic Algorithm; low-thrust; MGA; Optimization; Orbital Mechanics; Aerospace Engineering; Applied Mathematics

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APA (6th Edition):

Wagner, S. A. (2014). Automated trajectory design for impulsive and low thrust interplanetary mission analysis. (Thesis). Iowa State University. Retrieved from https://lib.dr.iastate.edu/etd/14238

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):

Wagner, Samuel Arthur. “Automated trajectory design for impulsive and low thrust interplanetary mission analysis.” 2014. Thesis, Iowa State University. Accessed January 21, 2021. https://lib.dr.iastate.edu/etd/14238.

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

MLA Handbook (7th Edition):

Wagner, Samuel Arthur. “Automated trajectory design for impulsive and low thrust interplanetary mission analysis.” 2014. Web. 21 Jan 2021.

Vancouver:

Wagner SA. Automated trajectory design for impulsive and low thrust interplanetary mission analysis. [Internet] [Thesis]. Iowa State University; 2014. [cited 2021 Jan 21]. Available from: https://lib.dr.iastate.edu/etd/14238.

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

Council of Science Editors:

Wagner SA. Automated trajectory design for impulsive and low thrust interplanetary mission analysis. [Thesis]. Iowa State University; 2014. Available from: https://lib.dr.iastate.edu/etd/14238

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


University of Arizona

14. Kidd, John Nocon. Development and Optimization of Low Energy Orbits for Advancing Exploration of the Solar System .

Degree: 2015, University of Arizona

 The architecture of a system which enables the cost-effective exploration of the solar system is proposed. Such a system will make use of the benefits… (more)

Subjects/Keywords: Interplanetary; Mission Design; Optimization; Orbital Mechanics; Spaceflight Dynamics; Systems & Industrial Engineering; Exploration Architecture

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APA (6th Edition):

Kidd, J. N. (2015). Development and Optimization of Low Energy Orbits for Advancing Exploration of the Solar System . (Masters Thesis). University of Arizona. Retrieved from http://hdl.handle.net/10150/560837

Chicago Manual of Style (16th Edition):

Kidd, John Nocon. “Development and Optimization of Low Energy Orbits for Advancing Exploration of the Solar System .” 2015. Masters Thesis, University of Arizona. Accessed January 21, 2021. http://hdl.handle.net/10150/560837.

MLA Handbook (7th Edition):

Kidd, John Nocon. “Development and Optimization of Low Energy Orbits for Advancing Exploration of the Solar System .” 2015. Web. 21 Jan 2021.

Vancouver:

Kidd JN. Development and Optimization of Low Energy Orbits for Advancing Exploration of the Solar System . [Internet] [Masters thesis]. University of Arizona; 2015. [cited 2021 Jan 21]. Available from: http://hdl.handle.net/10150/560837.

Council of Science Editors:

Kidd JN. Development and Optimization of Low Energy Orbits for Advancing Exploration of the Solar System . [Masters Thesis]. University of Arizona; 2015. Available from: http://hdl.handle.net/10150/560837

15. Gurgenburan, Goksel. A Methodology to Repair or Deorbit LEO Satellite Constellations.

Degree: MS, Mechanical & Aerospace Engineering, 2011, Old Dominion University

  In this thesis, mitigation of space debris is addressed by examining an approach for repair or de-orbit of a specific population of non-functional Low… (more)

Subjects/Keywords: Low Earth Orbit satellites; LEO; Clohessy-Wiltshire equations; Orbital mechanics; Aerospace Engineering

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APA (6th Edition):

Gurgenburan, G. (2011). A Methodology to Repair or Deorbit LEO Satellite Constellations. (Thesis). Old Dominion University. Retrieved from https://digitalcommons.odu.edu/mae_etds/318

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):

Gurgenburan, Goksel. “A Methodology to Repair or Deorbit LEO Satellite Constellations.” 2011. Thesis, Old Dominion University. Accessed January 21, 2021. https://digitalcommons.odu.edu/mae_etds/318.

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

MLA Handbook (7th Edition):

Gurgenburan, Goksel. “A Methodology to Repair or Deorbit LEO Satellite Constellations.” 2011. Web. 21 Jan 2021.

Vancouver:

Gurgenburan G. A Methodology to Repair or Deorbit LEO Satellite Constellations. [Internet] [Thesis]. Old Dominion University; 2011. [cited 2021 Jan 21]. Available from: https://digitalcommons.odu.edu/mae_etds/318.

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

Council of Science Editors:

Gurgenburan G. A Methodology to Repair or Deorbit LEO Satellite Constellations. [Thesis]. Old Dominion University; 2011. Available from: https://digitalcommons.odu.edu/mae_etds/318

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

16. Shepard, John. A Preliminary Study Of Leo To Geo Transfers For Inclination Changes Using Libration Point Orbits.

Degree: MS, Space Studies, 2020, University of North Dakota

  The required change in velocity for a satellite to change inclination has prompted studies of efficient orbital transfers. Modeling the motion of a spacecraft… (more)

Subjects/Keywords: CR3BP; invariant manifold; Libration Point Orbit; low-energy transfer; Lyapunov; orbital mechanics

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APA (6th Edition):

Shepard, J. (2020). A Preliminary Study Of Leo To Geo Transfers For Inclination Changes Using Libration Point Orbits. (Masters Thesis). University of North Dakota. Retrieved from https://commons.und.edu/theses/3121

Chicago Manual of Style (16th Edition):

Shepard, John. “A Preliminary Study Of Leo To Geo Transfers For Inclination Changes Using Libration Point Orbits.” 2020. Masters Thesis, University of North Dakota. Accessed January 21, 2021. https://commons.und.edu/theses/3121.

MLA Handbook (7th Edition):

Shepard, John. “A Preliminary Study Of Leo To Geo Transfers For Inclination Changes Using Libration Point Orbits.” 2020. Web. 21 Jan 2021.

Vancouver:

Shepard J. A Preliminary Study Of Leo To Geo Transfers For Inclination Changes Using Libration Point Orbits. [Internet] [Masters thesis]. University of North Dakota; 2020. [cited 2021 Jan 21]. Available from: https://commons.und.edu/theses/3121.

Council of Science Editors:

Shepard J. A Preliminary Study Of Leo To Geo Transfers For Inclination Changes Using Libration Point Orbits. [Masters Thesis]. University of North Dakota; 2020. Available from: https://commons.und.edu/theses/3121

17. Cognee, Kevin. Hybridization of open photonic resonators : Hybridation de résonateurs photoniques ouverts.

Degree: Docteur es, Lasers, Matière et Nanosciences, 2020, Bordeaux; Universiteit van Amsterdam

Le contrôle de l'interaction entre la lumière et la matière est d'une importance capitale dans de nombreuses technologies modernes, avec des applications allant de la… (more)

Subjects/Keywords: Modes quasi-Normaux; Hybrides metallo-Dielectriques; Moment orbital angulaire; Opto-Mécanique moléculaire; Coupled modes; Quasi-Normal modes; Orbital angular momentum; Molecular opto-Mechanics

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APA (6th Edition):

Cognee, K. (2020). Hybridization of open photonic resonators : Hybridation de résonateurs photoniques ouverts. (Doctoral Dissertation). Bordeaux; Universiteit van Amsterdam. Retrieved from http://www.theses.fr/2020BORD0002

Chicago Manual of Style (16th Edition):

Cognee, Kevin. “Hybridization of open photonic resonators : Hybridation de résonateurs photoniques ouverts.” 2020. Doctoral Dissertation, Bordeaux; Universiteit van Amsterdam. Accessed January 21, 2021. http://www.theses.fr/2020BORD0002.

MLA Handbook (7th Edition):

Cognee, Kevin. “Hybridization of open photonic resonators : Hybridation de résonateurs photoniques ouverts.” 2020. Web. 21 Jan 2021.

Vancouver:

Cognee K. Hybridization of open photonic resonators : Hybridation de résonateurs photoniques ouverts. [Internet] [Doctoral dissertation]. Bordeaux; Universiteit van Amsterdam; 2020. [cited 2021 Jan 21]. Available from: http://www.theses.fr/2020BORD0002.

Council of Science Editors:

Cognee K. Hybridization of open photonic resonators : Hybridation de résonateurs photoniques ouverts. [Doctoral Dissertation]. Bordeaux; Universiteit van Amsterdam; 2020. Available from: http://www.theses.fr/2020BORD0002


Texas A&M University

18. Read, Julie Louise. Modified Chebyshev Picard Iteration: Integration of Perturbed Motion using Modified Equinoctial Elements.

Degree: PhD, Aerospace Engineering, 2016, Texas A&M University

 The topic of this dissertation is the fusion of a novel integration method, Modified Chebyshev Picard Iteration (MCPI), with Gauss' Variational Equations using a set… (more)

Subjects/Keywords: Orbital Mechanics; Parallel Processing; Numerical Integration; Modified Chebyshev Picard Iteration; MCPI; Modified Equinoctial Elements; Chebyshev Polynomials

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

APA (6th Edition):

Read, J. L. (2016). Modified Chebyshev Picard Iteration: Integration of Perturbed Motion using Modified Equinoctial Elements. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/159095

Chicago Manual of Style (16th Edition):

Read, Julie Louise. “Modified Chebyshev Picard Iteration: Integration of Perturbed Motion using Modified Equinoctial Elements.” 2016. Doctoral Dissertation, Texas A&M University. Accessed January 21, 2021. http://hdl.handle.net/1969.1/159095.

MLA Handbook (7th Edition):

Read, Julie Louise. “Modified Chebyshev Picard Iteration: Integration of Perturbed Motion using Modified Equinoctial Elements.” 2016. Web. 21 Jan 2021.

Vancouver:

Read JL. Modified Chebyshev Picard Iteration: Integration of Perturbed Motion using Modified Equinoctial Elements. [Internet] [Doctoral dissertation]. Texas A&M University; 2016. [cited 2021 Jan 21]. Available from: http://hdl.handle.net/1969.1/159095.

Council of Science Editors:

Read JL. Modified Chebyshev Picard Iteration: Integration of Perturbed Motion using Modified Equinoctial Elements. [Doctoral Dissertation]. Texas A&M University; 2016. Available from: http://hdl.handle.net/1969.1/159095


Penn State University

19. Shank, Brian Steven. Development of an Optimized Lambert Problem Solver for Targeting Elliptical Orbits.

Degree: 2013, Penn State University

 This thesis investigates the solution of Lambert’s Problem for targets in elliptical orbits. Preliminary efforts are made in developing a mission design software tool to… (more)

Subjects/Keywords: Lambert's Problem; Pork Chop Plot; ATSV; Visual Data Techniques; Orbital Mechanics; Astrodynamics; Mission Planning; Propulsion Optimization

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APA (6th Edition):

Shank, B. S. (2013). Development of an Optimized Lambert Problem Solver for Targeting Elliptical Orbits. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/17560

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):

Shank, Brian Steven. “Development of an Optimized Lambert Problem Solver for Targeting Elliptical Orbits.” 2013. Thesis, Penn State University. Accessed January 21, 2021. https://submit-etda.libraries.psu.edu/catalog/17560.

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

MLA Handbook (7th Edition):

Shank, Brian Steven. “Development of an Optimized Lambert Problem Solver for Targeting Elliptical Orbits.” 2013. Web. 21 Jan 2021.

Vancouver:

Shank BS. Development of an Optimized Lambert Problem Solver for Targeting Elliptical Orbits. [Internet] [Thesis]. Penn State University; 2013. [cited 2021 Jan 21]. Available from: https://submit-etda.libraries.psu.edu/catalog/17560.

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

Council of Science Editors:

Shank BS. Development of an Optimized Lambert Problem Solver for Targeting Elliptical Orbits. [Thesis]. Penn State University; 2013. Available from: https://submit-etda.libraries.psu.edu/catalog/17560

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


University of Adelaide

20. Shimmin, Rogan. Trajectory design for a very-low-thrust lunar mission.

Degree: 2013, University of Adelaide

 The University of Stuttgart is conducting a research program to build a succession of small satellites. The ultimate goal of this program is to build… (more)

Subjects/Keywords: trajectory optimisation; trajectory design; orbital mechanics; space; spacecraft; simulation; modelling; low thrust; electric propulsion; ion thrusters

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APA (6th Edition):

Shimmin, R. (2013). Trajectory design for a very-low-thrust lunar mission. (Thesis). University of Adelaide. Retrieved from http://hdl.handle.net/2440/80842

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):

Shimmin, Rogan. “Trajectory design for a very-low-thrust lunar mission.” 2013. Thesis, University of Adelaide. Accessed January 21, 2021. http://hdl.handle.net/2440/80842.

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

MLA Handbook (7th Edition):

Shimmin, Rogan. “Trajectory design for a very-low-thrust lunar mission.” 2013. Web. 21 Jan 2021.

Vancouver:

Shimmin R. Trajectory design for a very-low-thrust lunar mission. [Internet] [Thesis]. University of Adelaide; 2013. [cited 2021 Jan 21]. Available from: http://hdl.handle.net/2440/80842.

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

Council of Science Editors:

Shimmin R. Trajectory design for a very-low-thrust lunar mission. [Thesis]. University of Adelaide; 2013. Available from: http://hdl.handle.net/2440/80842

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


Delft University of Technology

21. Molenaar, S. (author). Optimization of interplanetary trajectories with deep space maneuvers - Model development and application to a Uranus orbiter mission.

Degree: 2009, Delft University of Technology

Astrodynamics and Satellite Systems

Aerospace Engineering

Advisors/Committee Members: Noomen, R. (mentor).

Subjects/Keywords: Deep Space Maneuvers; Orbital Mechanics; Genetic Algorithm Optimization

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APA (6th Edition):

Molenaar, S. (. (2009). Optimization of interplanetary trajectories with deep space maneuvers - Model development and application to a Uranus orbiter mission. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:8d44eef0-1da0-47fa-b44e-cad4ab3e6a46

Chicago Manual of Style (16th Edition):

Molenaar, S (author). “Optimization of interplanetary trajectories with deep space maneuvers - Model development and application to a Uranus orbiter mission.” 2009. Masters Thesis, Delft University of Technology. Accessed January 21, 2021. http://resolver.tudelft.nl/uuid:8d44eef0-1da0-47fa-b44e-cad4ab3e6a46.

MLA Handbook (7th Edition):

Molenaar, S (author). “Optimization of interplanetary trajectories with deep space maneuvers - Model development and application to a Uranus orbiter mission.” 2009. Web. 21 Jan 2021.

Vancouver:

Molenaar S(. Optimization of interplanetary trajectories with deep space maneuvers - Model development and application to a Uranus orbiter mission. [Internet] [Masters thesis]. Delft University of Technology; 2009. [cited 2021 Jan 21]. Available from: http://resolver.tudelft.nl/uuid:8d44eef0-1da0-47fa-b44e-cad4ab3e6a46.

Council of Science Editors:

Molenaar S(. Optimization of interplanetary trajectories with deep space maneuvers - Model development and application to a Uranus orbiter mission. [Masters Thesis]. Delft University of Technology; 2009. Available from: http://resolver.tudelft.nl/uuid:8d44eef0-1da0-47fa-b44e-cad4ab3e6a46

22. Pousse, Alexandre. Le quasi-satellites et autres configurations remarquables en résonance co-orbitale : Around quasi-satellites and remarkable configurations in the co-orbital resonance.

Degree: Docteur es, Mécanique céleste, 2016, Paris Sciences et Lettres (ComUE)

L'ensemble des travaux menés au cours de cette thèse concerne l'étude de la résonance co-orbitale. Ce domaine de trajectoires particulières, où un astéroïde et une… (more)

Subjects/Keywords: Mécanique céleste; Résonance co-Orbitale; Problème à trois corps; Celestial mechanics; Co-Orbital resonance; Three-Body problem; 520

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APA (6th Edition):

Pousse, A. (2016). Le quasi-satellites et autres configurations remarquables en résonance co-orbitale : Around quasi-satellites and remarkable configurations in the co-orbital resonance. (Doctoral Dissertation). Paris Sciences et Lettres (ComUE). Retrieved from http://www.theses.fr/2016PSLEO006

Chicago Manual of Style (16th Edition):

Pousse, Alexandre. “Le quasi-satellites et autres configurations remarquables en résonance co-orbitale : Around quasi-satellites and remarkable configurations in the co-orbital resonance.” 2016. Doctoral Dissertation, Paris Sciences et Lettres (ComUE). Accessed January 21, 2021. http://www.theses.fr/2016PSLEO006.

MLA Handbook (7th Edition):

Pousse, Alexandre. “Le quasi-satellites et autres configurations remarquables en résonance co-orbitale : Around quasi-satellites and remarkable configurations in the co-orbital resonance.” 2016. Web. 21 Jan 2021.

Vancouver:

Pousse A. Le quasi-satellites et autres configurations remarquables en résonance co-orbitale : Around quasi-satellites and remarkable configurations in the co-orbital resonance. [Internet] [Doctoral dissertation]. Paris Sciences et Lettres (ComUE); 2016. [cited 2021 Jan 21]. Available from: http://www.theses.fr/2016PSLEO006.

Council of Science Editors:

Pousse A. Le quasi-satellites et autres configurations remarquables en résonance co-orbitale : Around quasi-satellites and remarkable configurations in the co-orbital resonance. [Doctoral Dissertation]. Paris Sciences et Lettres (ComUE); 2016. Available from: http://www.theses.fr/2016PSLEO006


Aristotle University Of Thessaloniki (AUTH); Αριστοτέλειο Πανεπιστήμιο Θεσσαλονίκης (ΑΠΘ)

23. Skoulidou, Despoina. Dynamical evolution of artificial satellites and space debris in near earth region.

Degree: 2019, Aristotle University Of Thessaloniki (AUTH); Αριστοτέλειο Πανεπιστήμιο Θεσσαλονίκης (ΑΠΘ)

In this study, we perform a complete, dynamical cartography of the dynamics of satellites and space debris in the near Earth space, by using detailed… (more)

Subjects/Keywords: Τροχιακή μηχανική; Τεχνητοί δορυφόροι; Διαστημικά κατάλοιπα; Εγγύς διαστημικό περιβάλλον; Orbital mechanics; Artificial satellites; Space debris; Near earth space environment

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APA (6th Edition):

Skoulidou, D. (2019). Dynamical evolution of artificial satellites and space debris in near earth region. (Thesis). Aristotle University Of Thessaloniki (AUTH); Αριστοτέλειο Πανεπιστήμιο Θεσσαλονίκης (ΑΠΘ). Retrieved from http://hdl.handle.net/10442/hedi/46490

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):

Skoulidou, Despoina. “Dynamical evolution of artificial satellites and space debris in near earth region.” 2019. Thesis, Aristotle University Of Thessaloniki (AUTH); Αριστοτέλειο Πανεπιστήμιο Θεσσαλονίκης (ΑΠΘ). Accessed January 21, 2021. http://hdl.handle.net/10442/hedi/46490.

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

MLA Handbook (7th Edition):

Skoulidou, Despoina. “Dynamical evolution of artificial satellites and space debris in near earth region.” 2019. Web. 21 Jan 2021.

Vancouver:

Skoulidou D. Dynamical evolution of artificial satellites and space debris in near earth region. [Internet] [Thesis]. Aristotle University Of Thessaloniki (AUTH); Αριστοτέλειο Πανεπιστήμιο Θεσσαλονίκης (ΑΠΘ); 2019. [cited 2021 Jan 21]. Available from: http://hdl.handle.net/10442/hedi/46490.

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

Council of Science Editors:

Skoulidou D. Dynamical evolution of artificial satellites and space debris in near earth region. [Thesis]. Aristotle University Of Thessaloniki (AUTH); Αριστοτέλειο Πανεπιστήμιο Θεσσαλονίκης (ΑΠΘ); 2019. Available from: http://hdl.handle.net/10442/hedi/46490

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


Rutgers University

24. Erb, Michael Philip, 1985-. The response of radiative feedbacks, equatorial Pacific seasonality, and wetlands to orbital forcing in model simulations.

Degree: Atmospheric Science, 2014, Rutgers University

Subjects/Keywords: Orbital mechanics; Radiative forcing; Climatic changes – Research

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APA (6th Edition):

Erb, Michael Philip, 1. (2014). The response of radiative feedbacks, equatorial Pacific seasonality, and wetlands to orbital forcing in model simulations. (Thesis). Rutgers University. Retrieved from https://rucore.libraries.rutgers.edu/rutgers-lib/42382/

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):

Erb, Michael Philip, 1985-. “The response of radiative feedbacks, equatorial Pacific seasonality, and wetlands to orbital forcing in model simulations.” 2014. Thesis, Rutgers University. Accessed January 21, 2021. https://rucore.libraries.rutgers.edu/rutgers-lib/42382/.

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

MLA Handbook (7th Edition):

Erb, Michael Philip, 1985-. “The response of radiative feedbacks, equatorial Pacific seasonality, and wetlands to orbital forcing in model simulations.” 2014. Web. 21 Jan 2021.

Vancouver:

Erb, Michael Philip 1. The response of radiative feedbacks, equatorial Pacific seasonality, and wetlands to orbital forcing in model simulations. [Internet] [Thesis]. Rutgers University; 2014. [cited 2021 Jan 21]. Available from: https://rucore.libraries.rutgers.edu/rutgers-lib/42382/.

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

Council of Science Editors:

Erb, Michael Philip 1. The response of radiative feedbacks, equatorial Pacific seasonality, and wetlands to orbital forcing in model simulations. [Thesis]. Rutgers University; 2014. Available from: https://rucore.libraries.rutgers.edu/rutgers-lib/42382/

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


The Ohio State University

25. Jedrey, Richard M. Development of a Discretized Model for the Restricted Three-Body Problem.

Degree: MS, Aero/Astro Engineering, 2011, The Ohio State University

 Spacecraft trajectory design is a science that requires high precision with little error. One of the most classic trajectory design problems is the restricted three-body… (more)

Subjects/Keywords: Aerospace Engineering; Engineering; orbital mechanics; spacecraft trajectories; three-body problem; three-body model; n-body problem; n-body model; discretized spacecraft

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APA (6th Edition):

Jedrey, R. M. (2011). Development of a Discretized Model for the Restricted Three-Body Problem. (Masters Thesis). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1306856595

Chicago Manual of Style (16th Edition):

Jedrey, Richard M. “Development of a Discretized Model for the Restricted Three-Body Problem.” 2011. Masters Thesis, The Ohio State University. Accessed January 21, 2021. http://rave.ohiolink.edu/etdc/view?acc_num=osu1306856595.

MLA Handbook (7th Edition):

Jedrey, Richard M. “Development of a Discretized Model for the Restricted Three-Body Problem.” 2011. Web. 21 Jan 2021.

Vancouver:

Jedrey RM. Development of a Discretized Model for the Restricted Three-Body Problem. [Internet] [Masters thesis]. The Ohio State University; 2011. [cited 2021 Jan 21]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1306856595.

Council of Science Editors:

Jedrey RM. Development of a Discretized Model for the Restricted Three-Body Problem. [Masters Thesis]. The Ohio State University; 2011. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1306856595


University of Cincinnati

26. SYED, ANEES. COLLISON PREDICTION AND AVOIDANCE OF SATELLITES IN FORMATION.

Degree: MS, Engineering : Mechanical Engineering, 2004, University of Cincinnati

 Satellites flying in formation has been the focus of current research. Sometimes,there are issues with the amount of information available about the satellites. Due to… (more)

Subjects/Keywords: satellites; satellite formations; formation control; orbital mechanics

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APA (6th Edition):

SYED, A. (2004). COLLISON PREDICTION AND AVOIDANCE OF SATELLITES IN FORMATION. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1100034591

Chicago Manual of Style (16th Edition):

SYED, ANEES. “COLLISON PREDICTION AND AVOIDANCE OF SATELLITES IN FORMATION.” 2004. Masters Thesis, University of Cincinnati. Accessed January 21, 2021. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1100034591.

MLA Handbook (7th Edition):

SYED, ANEES. “COLLISON PREDICTION AND AVOIDANCE OF SATELLITES IN FORMATION.” 2004. Web. 21 Jan 2021.

Vancouver:

SYED A. COLLISON PREDICTION AND AVOIDANCE OF SATELLITES IN FORMATION. [Internet] [Masters thesis]. University of Cincinnati; 2004. [cited 2021 Jan 21]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1100034591.

Council of Science Editors:

SYED A. COLLISON PREDICTION AND AVOIDANCE OF SATELLITES IN FORMATION. [Masters Thesis]. University of Cincinnati; 2004. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1100034591


Brno University of Technology

27. Stopka, Jiří. Program pro předpověď kolize Země s blízkými vesmírnými tělesy: Predictive software for Earth collision with Near Eartch Objects.

Degree: 2020, Brno University of Technology

 Aim of this bachelor’s thesis is to research and discuss the basics of orbital mechanics and their application on a real problem. The application of… (more)

Subjects/Keywords: Země; blízká vesmírná tělesa; Sluneční soustava; orbitální mechanika; Keplerovy zákony; Newtonův gravitační zákon; asteroidy; obežná dráha; kolize; elementy dráhy; Earth; Near-Earth Objects; Solar system; Orbital mechanics; Kepler’s laws; Newton’s law of universal gravitation; asteroids; orbit; collision; orbital elements

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APA (6th Edition):

Stopka, J. (2020). Program pro předpověď kolize Země s blízkými vesmírnými tělesy: Predictive software for Earth collision with Near Eartch Objects. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/192867

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):

Stopka, Jiří. “Program pro předpověď kolize Země s blízkými vesmírnými tělesy: Predictive software for Earth collision with Near Eartch Objects.” 2020. Thesis, Brno University of Technology. Accessed January 21, 2021. http://hdl.handle.net/11012/192867.

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

MLA Handbook (7th Edition):

Stopka, Jiří. “Program pro předpověď kolize Země s blízkými vesmírnými tělesy: Predictive software for Earth collision with Near Eartch Objects.” 2020. Web. 21 Jan 2021.

Vancouver:

Stopka J. Program pro předpověď kolize Země s blízkými vesmírnými tělesy: Predictive software for Earth collision with Near Eartch Objects. [Internet] [Thesis]. Brno University of Technology; 2020. [cited 2021 Jan 21]. Available from: http://hdl.handle.net/11012/192867.

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

Council of Science Editors:

Stopka J. Program pro předpověď kolize Země s blízkými vesmírnými tělesy: Predictive software for Earth collision with Near Eartch Objects. [Thesis]. Brno University of Technology; 2020. Available from: http://hdl.handle.net/11012/192867

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

28. Diaz, Christina R. A STUDY OF THE COLLISIONAL EVOLUTION OF ORBITAL DEBRIS IN GEOPOTENTIAL WELLS AND GEO DISPOSAL ORBITS.

Degree: MS, Aerospace Engineering, 2013, Cal Poly

  This thesis will present the effects of the orbital debris evolution in two key areas: the geosynchronous disposal orbit regime known as “graveyard” and… (more)

Subjects/Keywords: orbital debris; debris; collisions; ODPO; orbital mechanics; fortran; Astrodynamics; Other Aerospace Engineering

…overview of the orbital path of STK’s simulation and CDPROP’s simulation. STK is in blue while… …6.9 xi Chapter 1 Introduction and Background In terms of the space environment, orbital… …debris is a present and future hazard to all Earth space operations. Orbital debris consists of… …collisions also contribute to the present population. Orbital debris’ time in orbit is dependent on… …the orbital altitude. Debris in lower orbits often reenter within several years to decades… 

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APA (6th Edition):

Diaz, C. R. (2013). A STUDY OF THE COLLISIONAL EVOLUTION OF ORBITAL DEBRIS IN GEOPOTENTIAL WELLS AND GEO DISPOSAL ORBITS. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1063 ; 10.15368/theses.2013.157

Chicago Manual of Style (16th Edition):

Diaz, Christina R. “A STUDY OF THE COLLISIONAL EVOLUTION OF ORBITAL DEBRIS IN GEOPOTENTIAL WELLS AND GEO DISPOSAL ORBITS.” 2013. Masters Thesis, Cal Poly. Accessed January 21, 2021. https://digitalcommons.calpoly.edu/theses/1063 ; 10.15368/theses.2013.157.

MLA Handbook (7th Edition):

Diaz, Christina R. “A STUDY OF THE COLLISIONAL EVOLUTION OF ORBITAL DEBRIS IN GEOPOTENTIAL WELLS AND GEO DISPOSAL ORBITS.” 2013. Web. 21 Jan 2021.

Vancouver:

Diaz CR. A STUDY OF THE COLLISIONAL EVOLUTION OF ORBITAL DEBRIS IN GEOPOTENTIAL WELLS AND GEO DISPOSAL ORBITS. [Internet] [Masters thesis]. Cal Poly; 2013. [cited 2021 Jan 21]. Available from: https://digitalcommons.calpoly.edu/theses/1063 ; 10.15368/theses.2013.157.

Council of Science Editors:

Diaz CR. A STUDY OF THE COLLISIONAL EVOLUTION OF ORBITAL DEBRIS IN GEOPOTENTIAL WELLS AND GEO DISPOSAL ORBITS. [Masters Thesis]. Cal Poly; 2013. Available from: https://digitalcommons.calpoly.edu/theses/1063 ; 10.15368/theses.2013.157


Texas A&M University

29. Bourgeois, Scott K. Rock-Around Orbits.

Degree: MS, Aerospace Engineering, 2010, Texas A&M University

 The ability to observe resident space objects (RSOs) is a necessary requirement for space situational awareness. While objects in a Low-Earth Orbit are easily ob-… (more)

Subjects/Keywords: orbit; surveillance; orbital; dynamics; mechanics; geo; geostationary; geosynchronous; rock around; rock-around

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

APA (6th Edition):

Bourgeois, S. K. (2010). Rock-Around Orbits. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2009-12-7473

Chicago Manual of Style (16th Edition):

Bourgeois, Scott K. “Rock-Around Orbits.” 2010. Masters Thesis, Texas A&M University. Accessed January 21, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-2009-12-7473.

MLA Handbook (7th Edition):

Bourgeois, Scott K. “Rock-Around Orbits.” 2010. Web. 21 Jan 2021.

Vancouver:

Bourgeois SK. Rock-Around Orbits. [Internet] [Masters thesis]. Texas A&M University; 2010. [cited 2021 Jan 21]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2009-12-7473.

Council of Science Editors:

Bourgeois SK. Rock-Around Orbits. [Masters Thesis]. Texas A&M University; 2010. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2009-12-7473


University of Houston

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

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

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

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

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

APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Nallapu, Raviteja 1989-. “Orbit Propagation via MRQ Sphere Technique.” 2012. Masters Thesis, University of Houston. Accessed January 21, 2021. http://hdl.handle.net/10657/765.

MLA Handbook (7th Edition):

Nallapu, Raviteja 1989-. “Orbit Propagation via MRQ Sphere Technique.” 2012. Web. 21 Jan 2021.

Vancouver:

Nallapu R1. Orbit Propagation via MRQ Sphere Technique. [Internet] [Masters thesis]. University of Houston; 2012. [cited 2021 Jan 21]. 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

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