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You searched for subject:(SATELLITE ORBITS). Showing records 1 – 21 of 21 total matches.

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University of Florida

1. Carter, James B. Ad-Hoc Sub-Leo Cubesat Constellations Where Drag Is an Issue.

Degree: MS, Aerospace Engineering - Mechanical and Aerospace Engineering, 2015, University of Florida

 The objectives of this research were to explore the effect of atmospheric drag on ad-hoc CubeSat constellations in the sub-LEO space environment and to obtain… (more)

Subjects/Keywords: Altitude; Artificial satellites; Atmospherics; Circular orbits; Communications satellites; Constellations; Elliptical orbits; Low earth orbits; Orbits; Sensors; ad-hoc  – constellation  – cubesat  – satellite

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APA (6th Edition):

Carter, J. B. (2015). Ad-Hoc Sub-Leo Cubesat Constellations Where Drag Is an Issue. (Masters Thesis). University of Florida. Retrieved from https://ufdc.ufl.edu/UFE0048907

Chicago Manual of Style (16th Edition):

Carter, James B. “Ad-Hoc Sub-Leo Cubesat Constellations Where Drag Is an Issue.” 2015. Masters Thesis, University of Florida. Accessed October 31, 2020. https://ufdc.ufl.edu/UFE0048907.

MLA Handbook (7th Edition):

Carter, James B. “Ad-Hoc Sub-Leo Cubesat Constellations Where Drag Is an Issue.” 2015. Web. 31 Oct 2020.

Vancouver:

Carter JB. Ad-Hoc Sub-Leo Cubesat Constellations Where Drag Is an Issue. [Internet] [Masters thesis]. University of Florida; 2015. [cited 2020 Oct 31]. Available from: https://ufdc.ufl.edu/UFE0048907.

Council of Science Editors:

Carter JB. Ad-Hoc Sub-Leo Cubesat Constellations Where Drag Is an Issue. [Masters Thesis]. University of Florida; 2015. Available from: https://ufdc.ufl.edu/UFE0048907


University of Arizona

2. Reiland, Nathan. Assessing and Minimizing Collisions in Satellite Mega-Constellations .

Degree: 2020, University of Arizona

 The aim of this thesis is to provide satellite operators and researchers with an efficient means for evaluating and mitigating collision risk during the design… (more)

Subjects/Keywords: Dynamical evolution and stability; Frozen Orbits; Mega-Constellations; Satellite conjunction; Space debris

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APA (6th Edition):

Reiland, N. (2020). Assessing and Minimizing Collisions in Satellite Mega-Constellations . (Masters Thesis). University of Arizona. Retrieved from http://hdl.handle.net/10150/641658

Chicago Manual of Style (16th Edition):

Reiland, Nathan. “Assessing and Minimizing Collisions in Satellite Mega-Constellations .” 2020. Masters Thesis, University of Arizona. Accessed October 31, 2020. http://hdl.handle.net/10150/641658.

MLA Handbook (7th Edition):

Reiland, Nathan. “Assessing and Minimizing Collisions in Satellite Mega-Constellations .” 2020. Web. 31 Oct 2020.

Vancouver:

Reiland N. Assessing and Minimizing Collisions in Satellite Mega-Constellations . [Internet] [Masters thesis]. University of Arizona; 2020. [cited 2020 Oct 31]. Available from: http://hdl.handle.net/10150/641658.

Council of Science Editors:

Reiland N. Assessing and Minimizing Collisions in Satellite Mega-Constellations . [Masters Thesis]. University of Arizona; 2020. Available from: http://hdl.handle.net/10150/641658


University of Florida

3. Clark, Sheldon C. Design of a Representative Leo Satellite and Hypervelocity Impact Test to Improve the Nasa Standard Breakup Model.

Degree: MS, Aerospace Engineering - Mechanical and Aerospace Engineering, 2013, University of Florida

 The growth of the man made orbital debris population poses accelerating risk to the operational safety of both manned and unmanned space assets. Several government… (more)

Subjects/Keywords: Aluminum; Artificial satellites; Avionics; Hypervelocity impact; Low earth orbits; Modeling; Orbits; Payloads; Satellite design; Space debris; airforce  – collision  – debris  – debrisat  – hypervelocity  – impact  – nasa  – orbital

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APA (6th Edition):

Clark, S. C. (2013). Design of a Representative Leo Satellite and Hypervelocity Impact Test to Improve the Nasa Standard Breakup Model. (Masters Thesis). University of Florida. Retrieved from https://ufdc.ufl.edu/UFE0045626

Chicago Manual of Style (16th Edition):

Clark, Sheldon C. “Design of a Representative Leo Satellite and Hypervelocity Impact Test to Improve the Nasa Standard Breakup Model.” 2013. Masters Thesis, University of Florida. Accessed October 31, 2020. https://ufdc.ufl.edu/UFE0045626.

MLA Handbook (7th Edition):

Clark, Sheldon C. “Design of a Representative Leo Satellite and Hypervelocity Impact Test to Improve the Nasa Standard Breakup Model.” 2013. Web. 31 Oct 2020.

Vancouver:

Clark SC. Design of a Representative Leo Satellite and Hypervelocity Impact Test to Improve the Nasa Standard Breakup Model. [Internet] [Masters thesis]. University of Florida; 2013. [cited 2020 Oct 31]. Available from: https://ufdc.ufl.edu/UFE0045626.

Council of Science Editors:

Clark SC. Design of a Representative Leo Satellite and Hypervelocity Impact Test to Improve the Nasa Standard Breakup Model. [Masters Thesis]. University of Florida; 2013. Available from: https://ufdc.ufl.edu/UFE0045626


Penn State University

4. Williams, Patrick. Using Numerical Optimization Techniques and General Perturbation Equations to Find Optimal Near-Earth Orbit Transfers.

Degree: 2009, Penn State University

 With recent developments in low-thrust optimization techniques, several methods of trajectory optimization can be implemented across various transfers. Much recent work has focused on performing… (more)

Subjects/Keywords: Low-thrust; Optimization; Molniya Orbits; Evolutionary Comuptation; Satellite Toolkit

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APA (6th Edition):

Williams, P. (2009). Using Numerical Optimization Techniques and General Perturbation Equations to Find Optimal Near-Earth Orbit Transfers. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/9593

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):

Williams, Patrick. “Using Numerical Optimization Techniques and General Perturbation Equations to Find Optimal Near-Earth Orbit Transfers.” 2009. Thesis, Penn State University. Accessed October 31, 2020. https://submit-etda.libraries.psu.edu/catalog/9593.

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

MLA Handbook (7th Edition):

Williams, Patrick. “Using Numerical Optimization Techniques and General Perturbation Equations to Find Optimal Near-Earth Orbit Transfers.” 2009. Web. 31 Oct 2020.

Vancouver:

Williams P. Using Numerical Optimization Techniques and General Perturbation Equations to Find Optimal Near-Earth Orbit Transfers. [Internet] [Thesis]. Penn State University; 2009. [cited 2020 Oct 31]. Available from: https://submit-etda.libraries.psu.edu/catalog/9593.

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

Council of Science Editors:

Williams P. Using Numerical Optimization Techniques and General Perturbation Equations to Find Optimal Near-Earth Orbit Transfers. [Thesis]. Penn State University; 2009. Available from: https://submit-etda.libraries.psu.edu/catalog/9593

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

5. Pedroso, Pedro António de Sousa. Radio, satellite communications and tracking station.

Degree: 2016, RCAAP

Esta dissertação descreve o trabalho desenvolvido para montar uma estação de rádio para comunicações via satélite e a sua aplicação no meio académico e de… (more)

Subjects/Keywords: Estação de rádio; Comunicação; Satellite communications; Radio station; Orbits; Tracking; Control; Radio navigation; Domínio/Área Científica::Engenharia e Tecnologia

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APA (6th Edition):

Pedroso, P. A. d. S. (2016). Radio, satellite communications and tracking station. (Thesis). RCAAP. Retrieved from https://www.rcaap.pt/detail.jsp?id=oai:repositorio.iscte-iul.pt:10071/12783

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):

Pedroso, Pedro António de Sousa. “Radio, satellite communications and tracking station.” 2016. Thesis, RCAAP. Accessed October 31, 2020. https://www.rcaap.pt/detail.jsp?id=oai:repositorio.iscte-iul.pt:10071/12783.

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

MLA Handbook (7th Edition):

Pedroso, Pedro António de Sousa. “Radio, satellite communications and tracking station.” 2016. Web. 31 Oct 2020.

Vancouver:

Pedroso PAdS. Radio, satellite communications and tracking station. [Internet] [Thesis]. RCAAP; 2016. [cited 2020 Oct 31]. Available from: https://www.rcaap.pt/detail.jsp?id=oai:repositorio.iscte-iul.pt:10071/12783.

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

Council of Science Editors:

Pedroso PAdS. Radio, satellite communications and tracking station. [Thesis]. RCAAP; 2016. Available from: https://www.rcaap.pt/detail.jsp?id=oai:repositorio.iscte-iul.pt:10071/12783

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


University of Florida

6. Allgeier, Shawn E. Determination of Motion Extrema in Multi-Satellite Systems.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2011, University of Florida

 Spacecraft, or satellite formation flight has been a topic of interest dating back to the Gemini program of the 1960s. Traditionally space missions have been… (more)

Subjects/Keywords: Algebra; Artificial satellites; Distance functions; Extrema; Orbitals; Orbits; Polynomials; Sine function; Spacecraft; Velocity; astrodynamics  – extrema  – formation  – groebner  – multi-body  – satellite

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APA (6th Edition):

Allgeier, S. E. (2011). Determination of Motion Extrema in Multi-Satellite Systems. (Doctoral Dissertation). University of Florida. Retrieved from https://ufdc.ufl.edu/UFE0043286

Chicago Manual of Style (16th Edition):

Allgeier, Shawn E. “Determination of Motion Extrema in Multi-Satellite Systems.” 2011. Doctoral Dissertation, University of Florida. Accessed October 31, 2020. https://ufdc.ufl.edu/UFE0043286.

MLA Handbook (7th Edition):

Allgeier, Shawn E. “Determination of Motion Extrema in Multi-Satellite Systems.” 2011. Web. 31 Oct 2020.

Vancouver:

Allgeier SE. Determination of Motion Extrema in Multi-Satellite Systems. [Internet] [Doctoral dissertation]. University of Florida; 2011. [cited 2020 Oct 31]. Available from: https://ufdc.ufl.edu/UFE0043286.

Council of Science Editors:

Allgeier SE. Determination of Motion Extrema in Multi-Satellite Systems. [Doctoral Dissertation]. University of Florida; 2011. Available from: https://ufdc.ufl.edu/UFE0043286


Montana State University

7. Solomon, Dylan Raymond. Analysis and design of the mechanical systems onboard a microsatellite in low-earth orbit : an assessment study.

Degree: MS, College of Engineering, 2005, Montana State University

 A study of the mechanical systems contributing to the design and performance of a picosatellite's mission in low-Earth orbit (LEO) was performed through design and… (more)

Subjects/Keywords: Cosmos (Artificial satellite); Artificial satellites Orbits.; Artificial satellites Thermodynamics.

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APA (6th Edition):

Solomon, D. R. (2005). Analysis and design of the mechanical systems onboard a microsatellite in low-earth orbit : an assessment study. (Masters Thesis). Montana State University. Retrieved from https://scholarworks.montana.edu/xmlui/handle/1/2323

Chicago Manual of Style (16th Edition):

Solomon, Dylan Raymond. “Analysis and design of the mechanical systems onboard a microsatellite in low-earth orbit : an assessment study.” 2005. Masters Thesis, Montana State University. Accessed October 31, 2020. https://scholarworks.montana.edu/xmlui/handle/1/2323.

MLA Handbook (7th Edition):

Solomon, Dylan Raymond. “Analysis and design of the mechanical systems onboard a microsatellite in low-earth orbit : an assessment study.” 2005. Web. 31 Oct 2020.

Vancouver:

Solomon DR. Analysis and design of the mechanical systems onboard a microsatellite in low-earth orbit : an assessment study. [Internet] [Masters thesis]. Montana State University; 2005. [cited 2020 Oct 31]. Available from: https://scholarworks.montana.edu/xmlui/handle/1/2323.

Council of Science Editors:

Solomon DR. Analysis and design of the mechanical systems onboard a microsatellite in low-earth orbit : an assessment study. [Masters Thesis]. Montana State University; 2005. Available from: https://scholarworks.montana.edu/xmlui/handle/1/2323


University of Florida

8. Werremeyer, Mark R. Design of Subsystems for a Representative Modern LEO Satellite.

Degree: MS, Aerospace Engineering - Mechanical and Aerospace Engineering, 2013, University of Florida

 This thesis discusses the design of subsystems for a representative modern low Earth Orbit (LEO) satellite. Specifically, the subsystems presented were designed for inclusion on… (more)

Subjects/Keywords: Aluminum; Artificial satellites; Composite materials; Low earth orbits; Magnetism; Nadir; Plumbing; Propulsion; Satellite design; Thrusters; attitude  – debris  – debrisat  – hypervelocity  – impact  – leo  – modern  – orbital  – propulsion  – representative  – satellite  – structure  – subsystems  – test  – thermal

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APA (6th Edition):

Werremeyer, M. R. (2013). Design of Subsystems for a Representative Modern LEO Satellite. (Masters Thesis). University of Florida. Retrieved from https://ufdc.ufl.edu/UFE0045534

Chicago Manual of Style (16th Edition):

Werremeyer, Mark R. “Design of Subsystems for a Representative Modern LEO Satellite.” 2013. Masters Thesis, University of Florida. Accessed October 31, 2020. https://ufdc.ufl.edu/UFE0045534.

MLA Handbook (7th Edition):

Werremeyer, Mark R. “Design of Subsystems for a Representative Modern LEO Satellite.” 2013. Web. 31 Oct 2020.

Vancouver:

Werremeyer MR. Design of Subsystems for a Representative Modern LEO Satellite. [Internet] [Masters thesis]. University of Florida; 2013. [cited 2020 Oct 31]. Available from: https://ufdc.ufl.edu/UFE0045534.

Council of Science Editors:

Werremeyer MR. Design of Subsystems for a Representative Modern LEO Satellite. [Masters Thesis]. University of Florida; 2013. Available from: https://ufdc.ufl.edu/UFE0045534


The Ohio State University

9. Habana, Nlingilili Oarabile Kgosietsile. Gravity Recovery by Kinematic State Vector Perturbation from Satellite-to-Satellite Tracking for GRACE-like Orbits over Long Arcs.

Degree: PhD, Geodetic Science, 2020, The Ohio State University

 To improve on the understanding of Earth dynamics, a perturbation theory aimed at geopotential recovery, based on purely kinematic state vectors, is implemented. The method… (more)

Subjects/Keywords: Applied Mathematics; Geophysical; Earth; Geophysics; Statistics; gravitation; SST; GRACE; perturbation theory; long arcs; kinematic orbits; satellite-to-satellite tracking; gravity recovery; spherical harmonic estimation

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APA (6th Edition):

Habana, N. O. K. (2020). Gravity Recovery by Kinematic State Vector Perturbation from Satellite-to-Satellite Tracking for GRACE-like Orbits over Long Arcs. (Doctoral Dissertation). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1578042687104082

Chicago Manual of Style (16th Edition):

Habana, Nlingilili Oarabile Kgosietsile. “Gravity Recovery by Kinematic State Vector Perturbation from Satellite-to-Satellite Tracking for GRACE-like Orbits over Long Arcs.” 2020. Doctoral Dissertation, The Ohio State University. Accessed October 31, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=osu1578042687104082.

MLA Handbook (7th Edition):

Habana, Nlingilili Oarabile Kgosietsile. “Gravity Recovery by Kinematic State Vector Perturbation from Satellite-to-Satellite Tracking for GRACE-like Orbits over Long Arcs.” 2020. Web. 31 Oct 2020.

Vancouver:

Habana NOK. Gravity Recovery by Kinematic State Vector Perturbation from Satellite-to-Satellite Tracking for GRACE-like Orbits over Long Arcs. [Internet] [Doctoral dissertation]. The Ohio State University; 2020. [cited 2020 Oct 31]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1578042687104082.

Council of Science Editors:

Habana NOK. Gravity Recovery by Kinematic State Vector Perturbation from Satellite-to-Satellite Tracking for GRACE-like Orbits over Long Arcs. [Doctoral Dissertation]. The Ohio State University; 2020. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1578042687104082


Stellenbosch University

10. Du Plessis, Jan Abraham Francois. Low earth orbit satellite propagators.

Degree: M.Ing., Electrical and Electronic Engineering, 1999, Stellenbosch University

ENGLISH ABSTRACT: The objective of this study was to implement an orbital propagation algorithm, which could be used for the purpose of mission planning and… (more)

Subjects/Keywords: Orbits; Artificial satellites; Dissertations  – Electronic engineering; Satellite orbit predictions; Orbit determination algorithms

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APA (6th Edition):

Du Plessis, J. A. F. (1999). Low earth orbit satellite propagators. (Masters Thesis). Stellenbosch University. Retrieved from http://hdl.handle.net/10019.1/51326

Chicago Manual of Style (16th Edition):

Du Plessis, Jan Abraham Francois. “Low earth orbit satellite propagators.” 1999. Masters Thesis, Stellenbosch University. Accessed October 31, 2020. http://hdl.handle.net/10019.1/51326.

MLA Handbook (7th Edition):

Du Plessis, Jan Abraham Francois. “Low earth orbit satellite propagators.” 1999. Web. 31 Oct 2020.

Vancouver:

Du Plessis JAF. Low earth orbit satellite propagators. [Internet] [Masters thesis]. Stellenbosch University; 1999. [cited 2020 Oct 31]. Available from: http://hdl.handle.net/10019.1/51326.

Council of Science Editors:

Du Plessis JAF. Low earth orbit satellite propagators. [Masters Thesis]. Stellenbosch University; 1999. Available from: http://hdl.handle.net/10019.1/51326


University of Florida

11. Muri, Paul D. Delay Tolerant Networking for Cubesat Topologies and Platforms.

Degree: PhD, Electrical and Computer Engineering, 2013, University of Florida

 A CubeSat is a pico satellite platform with a volume as small as 10cm3. Universities, companies, and governments launch CubeSats for individual technology experiments, demonstrations, and research… (more)

Subjects/Keywords: Antennas; Artificial satellites; Communication systems; Communications satellites; Constellations; Earth stations; Helical antennas; Low earth orbits; Simulations; Topology; antennas  – communications  – cubesat  – emulation  – networking  – satellite  – simulation  – topology

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APA (6th Edition):

Muri, P. D. (2013). Delay Tolerant Networking for Cubesat Topologies and Platforms. (Doctoral Dissertation). University of Florida. Retrieved from https://ufdc.ufl.edu/UFE0045864

Chicago Manual of Style (16th Edition):

Muri, Paul D. “Delay Tolerant Networking for Cubesat Topologies and Platforms.” 2013. Doctoral Dissertation, University of Florida. Accessed October 31, 2020. https://ufdc.ufl.edu/UFE0045864.

MLA Handbook (7th Edition):

Muri, Paul D. “Delay Tolerant Networking for Cubesat Topologies and Platforms.” 2013. Web. 31 Oct 2020.

Vancouver:

Muri PD. Delay Tolerant Networking for Cubesat Topologies and Platforms. [Internet] [Doctoral dissertation]. University of Florida; 2013. [cited 2020 Oct 31]. Available from: https://ufdc.ufl.edu/UFE0045864.

Council of Science Editors:

Muri PD. Delay Tolerant Networking for Cubesat Topologies and Platforms. [Doctoral Dissertation]. University of Florida; 2013. Available from: https://ufdc.ufl.edu/UFE0045864

12. Hoskins, Aaron Bradley. Best longitudinal adjustment of satellite trajectories for the observation of forest fires (BLASTOFF): A stochastic programming approach to satellite system design.

Degree: PhD, Industrial and Systems Engineering, 2017, Mississippi State University

  Forest fires cause a significant amount of damage and destruction each year. Optimally dispatching resources reduces the amount of damage a forest fire can… (more)

Subjects/Keywords: Initial Satellite Orbits; Satellite Maneuvers; Satellite Ground Stations; Stochastic Programming; L-shaped Method; Sample Average Approximation; Forest Fires; Disaster Response

…changing satellite missions is an active area of research. Designing initial orbits that can… …Satellite Data Collection Scheduling 2.2.2 Orbit Design . . . . . . . . . . . . . 2.2.3 Satellite… …Maneuvering . . . . . . . . 2.2.4 Satellite Collection of Disaster Data 2.2.5 Disaster Preparedness… …Ascending and Descending-Passes . . . . . . . . . . . . . . . . . . . . . . 87 5.1 Satellite… …Uploads Disaster Data from Yellowstone Disaster Site. . . . . . . 122 5.2 Satellite Downloads… 

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APA (6th Edition):

Hoskins, A. B. (2017). Best longitudinal adjustment of satellite trajectories for the observation of forest fires (BLASTOFF): A stochastic programming approach to satellite system design. (Doctoral Dissertation). Mississippi State University. Retrieved from http://sun.library.msstate.edu/ETD-db/theses/available/etd-03182017-150019/ ;

Chicago Manual of Style (16th Edition):

Hoskins, Aaron Bradley. “Best longitudinal adjustment of satellite trajectories for the observation of forest fires (BLASTOFF): A stochastic programming approach to satellite system design.” 2017. Doctoral Dissertation, Mississippi State University. Accessed October 31, 2020. http://sun.library.msstate.edu/ETD-db/theses/available/etd-03182017-150019/ ;.

MLA Handbook (7th Edition):

Hoskins, Aaron Bradley. “Best longitudinal adjustment of satellite trajectories for the observation of forest fires (BLASTOFF): A stochastic programming approach to satellite system design.” 2017. Web. 31 Oct 2020.

Vancouver:

Hoskins AB. Best longitudinal adjustment of satellite trajectories for the observation of forest fires (BLASTOFF): A stochastic programming approach to satellite system design. [Internet] [Doctoral dissertation]. Mississippi State University; 2017. [cited 2020 Oct 31]. Available from: http://sun.library.msstate.edu/ETD-db/theses/available/etd-03182017-150019/ ;.

Council of Science Editors:

Hoskins AB. Best longitudinal adjustment of satellite trajectories for the observation of forest fires (BLASTOFF): A stochastic programming approach to satellite system design. [Doctoral Dissertation]. Mississippi State University; 2017. Available from: http://sun.library.msstate.edu/ETD-db/theses/available/etd-03182017-150019/ ;

13. Aubin, Brianna S. Optimization of relative orbit transfers via particle swarm and primer vector theory.

Degree: MS, 4048, 2011, University of Illinois – Urbana-Champaign

Satellite clusters are a useful tool to improve mission cost-effectiveness and redundancy, but controlling the satellites within the cluster is a difficult task. The particle… (more)

Subjects/Keywords: relative orbits; Clohessy Wiltshire; primer vector; particle swarm; relative orbit elements; evolutionary algorithms; satellite swarm

…Earth oblateness viii Chapter 1: Introduction 1.1 The Use of Satellite Clusters Rather… …than flying a single massive satellite in order to accomplish a mission, it is sometimes… …beneficial to fly many smaller satellites in similar orbits in order to form a „cluster‟ of… …problem in the use of satellite clusters that needs to be addressed is accurately controlling… …smaller fuel requirements allow more of the satellite's mass to be devoted to other… 

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APA (6th Edition):

Aubin, B. S. (2011). Optimization of relative orbit transfers via particle swarm and primer vector theory. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/24011

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):

Aubin, Brianna S. “Optimization of relative orbit transfers via particle swarm and primer vector theory.” 2011. Thesis, University of Illinois – Urbana-Champaign. Accessed October 31, 2020. http://hdl.handle.net/2142/24011.

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

MLA Handbook (7th Edition):

Aubin, Brianna S. “Optimization of relative orbit transfers via particle swarm and primer vector theory.” 2011. Web. 31 Oct 2020.

Vancouver:

Aubin BS. Optimization of relative orbit transfers via particle swarm and primer vector theory. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2011. [cited 2020 Oct 31]. Available from: http://hdl.handle.net/2142/24011.

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

Council of Science Editors:

Aubin BS. Optimization of relative orbit transfers via particle swarm and primer vector theory. [Thesis]. University of Illinois – Urbana-Champaign; 2011. Available from: http://hdl.handle.net/2142/24011

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


Georgia Tech

14. Salazar Kardozo, Alexandros. A High-Level Framework for the Autonomous Refueling of Satellite Constellations.

Degree: MS, Aerospace Engineering, 2007, Georgia Tech

Satellite constellations are an increasingly attractive option for many commercial and military applications. They provide a robust and distributed method of accomplishing the goals of… (more)

Subjects/Keywords: Scheduling; Auction algorithms; Optimization; Satellite constellations; Artificial satellites Orbits Mathematical models; Artificial satellites Maintenance and repair

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APA (6th Edition):

Salazar Kardozo, A. (2007). A High-Level Framework for the Autonomous Refueling of Satellite Constellations. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/14534

Chicago Manual of Style (16th Edition):

Salazar Kardozo, Alexandros. “A High-Level Framework for the Autonomous Refueling of Satellite Constellations.” 2007. Masters Thesis, Georgia Tech. Accessed October 31, 2020. http://hdl.handle.net/1853/14534.

MLA Handbook (7th Edition):

Salazar Kardozo, Alexandros. “A High-Level Framework for the Autonomous Refueling of Satellite Constellations.” 2007. Web. 31 Oct 2020.

Vancouver:

Salazar Kardozo A. A High-Level Framework for the Autonomous Refueling of Satellite Constellations. [Internet] [Masters thesis]. Georgia Tech; 2007. [cited 2020 Oct 31]. Available from: http://hdl.handle.net/1853/14534.

Council of Science Editors:

Salazar Kardozo A. A High-Level Framework for the Autonomous Refueling of Satellite Constellations. [Masters Thesis]. Georgia Tech; 2007. Available from: http://hdl.handle.net/1853/14534


University of Florida

15. Cojuangco, Ai-Ai Lumnay C. Orbital Lifetime Analyses of Pico- and Nano-Satellites.

Degree: MS, Mechanical Engineering - Mechanical and Aerospace Engineering, 2007, University of Florida

 In recent years, orbital debris has been a growing concern for the space industry due to its potential risk of causing collisions. Several agencies and… (more)

Subjects/Keywords: Altitude; Artificial satellites; Atmospheric density; Drag coefficient; Orbital elements; Orbital lifetime; Orbitals; Orbits; Simulations; Space debris; lifetime, nano, orbital, pico, satellite

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

APA (6th Edition):

Cojuangco, A. L. C. (2007). Orbital Lifetime Analyses of Pico- and Nano-Satellites. (Masters Thesis). University of Florida. Retrieved from https://ufdc.ufl.edu/UFE0020154

Chicago Manual of Style (16th Edition):

Cojuangco, Ai-Ai Lumnay C. “Orbital Lifetime Analyses of Pico- and Nano-Satellites.” 2007. Masters Thesis, University of Florida. Accessed October 31, 2020. https://ufdc.ufl.edu/UFE0020154.

MLA Handbook (7th Edition):

Cojuangco, Ai-Ai Lumnay C. “Orbital Lifetime Analyses of Pico- and Nano-Satellites.” 2007. Web. 31 Oct 2020.

Vancouver:

Cojuangco ALC. Orbital Lifetime Analyses of Pico- and Nano-Satellites. [Internet] [Masters thesis]. University of Florida; 2007. [cited 2020 Oct 31]. Available from: https://ufdc.ufl.edu/UFE0020154.

Council of Science Editors:

Cojuangco ALC. Orbital Lifetime Analyses of Pico- and Nano-Satellites. [Masters Thesis]. University of Florida; 2007. Available from: https://ufdc.ufl.edu/UFE0020154

16. ΧΑΤΖΗΦΩΤΕΙΝΟΥ, ΑΙΚΑΤΕΡΙΝΗ. ΤΡΙΔΙΑΣΤΑΤΑ ΑΡΙΘΜΗΤΙΚΑ ΜΟΝΤΕΛΑ ΟΛΟΚΛΗΡΩΣΗΣ ΠΛΑΝΗΤΙΚΩΝ ΚΑΙ ΔΟΡΥΦΟΡΙΚΩΝ ΤΡΟΧΙΩΝ.

Degree: 1998, Αριστοτέλειο Πανεπιστήμιο Θεσσαλονίκης (ΑΠΘ); Aristotle University Of Thessaloniki (AUTH)

Η ΠΑΡΟΥΣΑ ΔΙΑΤΡΙΒΗ ΕΧΕΙ ΩΣ ΑΝΤΙΚΕΙΜΕΝΟ ΤΗΝ ΑΝΑΠΤΥΞΗ ΑΡΙΘΜΗΤΙΚΩΝ ΚΑΙ ΗΜΙ-ΑΝΑΛΥΤΙΚΩΝ ΜΕΘΟΔΩΝ ΓΙΑ ΤΗΝ ΕΠΙΛΥΣΗ ΣΥΓΧΡΟΝΩΝ ΠΡΟΒΛΗΜΑΤΩΝ ΟΥΡΑΝΙΑΣ ΜΗΧΑΝΙΚΗΣ. ΣΤΟ ΠΡΩΤΟ ΚΕΦΑΛΑΙΟ ΑΝΑΠΤΥΣΣΕΤΑΙ ΜΙΑ ΝΕΑ… (more)

Subjects/Keywords: CELESTIAL MECHANICS; Chaos; Numerical integration; Numerical methods; ORBITAL STABILITY; PLANETARY ORBITS; SATELLITE ORBITS; SYMPLECTIC MAPPINGS; Αριθμητικές μέθοδοι; Αριθμητική ολοκλήρωση; ΔΟΡΥΦΟΡΙΚΕΣ ΤΡΟΧΙΕΣ; ΕΥΣΤΑΘΕΙΑ ΤΡΟΧΙΩΝ; Ουράνια μηχανική; ΠΛΑΝΗΤΙΚΕΣ ΤΡΟΧΙΕΣ; Συμπλεκτικές απεικονίσεις; Χάος

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APA (6th Edition):

ΧΑΤΖΗΦΩΤΕΙΝΟΥ, . (1998). ΤΡΙΔΙΑΣΤΑΤΑ ΑΡΙΘΜΗΤΙΚΑ ΜΟΝΤΕΛΑ ΟΛΟΚΛΗΡΩΣΗΣ ΠΛΑΝΗΤΙΚΩΝ ΚΑΙ ΔΟΡΥΦΟΡΙΚΩΝ ΤΡΟΧΙΩΝ. (Thesis). Αριστοτέλειο Πανεπιστήμιο Θεσσαλονίκης (ΑΠΘ); Aristotle University Of Thessaloniki (AUTH). Retrieved from http://hdl.handle.net/10442/hedi/10666

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):

ΧΑΤΖΗΦΩΤΕΙΝΟΥ, ΑΙΚΑΤΕΡΙΝΗ. “ΤΡΙΔΙΑΣΤΑΤΑ ΑΡΙΘΜΗΤΙΚΑ ΜΟΝΤΕΛΑ ΟΛΟΚΛΗΡΩΣΗΣ ΠΛΑΝΗΤΙΚΩΝ ΚΑΙ ΔΟΡΥΦΟΡΙΚΩΝ ΤΡΟΧΙΩΝ.” 1998. Thesis, Αριστοτέλειο Πανεπιστήμιο Θεσσαλονίκης (ΑΠΘ); Aristotle University Of Thessaloniki (AUTH). Accessed October 31, 2020. http://hdl.handle.net/10442/hedi/10666.

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

MLA Handbook (7th Edition):

ΧΑΤΖΗΦΩΤΕΙΝΟΥ, ΑΙΚΑΤΕΡΙΝΗ. “ΤΡΙΔΙΑΣΤΑΤΑ ΑΡΙΘΜΗΤΙΚΑ ΜΟΝΤΕΛΑ ΟΛΟΚΛΗΡΩΣΗΣ ΠΛΑΝΗΤΙΚΩΝ ΚΑΙ ΔΟΡΥΦΟΡΙΚΩΝ ΤΡΟΧΙΩΝ.” 1998. Web. 31 Oct 2020.

Vancouver:

ΧΑΤΖΗΦΩΤΕΙΝΟΥ . ΤΡΙΔΙΑΣΤΑΤΑ ΑΡΙΘΜΗΤΙΚΑ ΜΟΝΤΕΛΑ ΟΛΟΚΛΗΡΩΣΗΣ ΠΛΑΝΗΤΙΚΩΝ ΚΑΙ ΔΟΡΥΦΟΡΙΚΩΝ ΤΡΟΧΙΩΝ. [Internet] [Thesis]. Αριστοτέλειο Πανεπιστήμιο Θεσσαλονίκης (ΑΠΘ); Aristotle University Of Thessaloniki (AUTH); 1998. [cited 2020 Oct 31]. Available from: http://hdl.handle.net/10442/hedi/10666.

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

Council of Science Editors:

ΧΑΤΖΗΦΩΤΕΙΝΟΥ . ΤΡΙΔΙΑΣΤΑΤΑ ΑΡΙΘΜΗΤΙΚΑ ΜΟΝΤΕΛΑ ΟΛΟΚΛΗΡΩΣΗΣ ΠΛΑΝΗΤΙΚΩΝ ΚΑΙ ΔΟΡΥΦΟΡΙΚΩΝ ΤΡΟΧΙΩΝ. [Thesis]. Αριστοτέλειο Πανεπιστήμιο Θεσσαλονίκης (ΑΠΘ); Aristotle University Of Thessaloniki (AUTH); 1998. Available from: http://hdl.handle.net/10442/hedi/10666

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

17. Hélio Koiti Kuga. Estimação adaptativa de órbitas aplicada a satélites a baixa altitude.

Degree: 1981, Instituto Nacional de Pesquisas Espaciais

Os procedimentos de estimação são implementados e testados, com o objetivo de verificar a possibilidade de sua utilização na terminação de órbita, em tempo real,… (more)

Subjects/Keywords: determinação de órbita; filtro de Kalman; estimação adaptativa; low altitude; orbital position estimation; satellite orbits; digital simulation; real time operation; orbit determination; Kalman filter; adaptive estimation

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

APA (6th Edition):

Kuga, H. K. (1981). Estimação adaptativa de órbitas aplicada a satélites a baixa altitude. (Thesis). Instituto Nacional de Pesquisas Espaciais. Retrieved from http://urlib.net/sid.inpe.br/[email protected]/2005/07.27.13.52

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):

Kuga, Hélio Koiti. “Estimação adaptativa de órbitas aplicada a satélites a baixa altitude.” 1981. Thesis, Instituto Nacional de Pesquisas Espaciais. Accessed October 31, 2020. http://urlib.net/sid.inpe.br/[email protected]/2005/07.27.13.52.

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

MLA Handbook (7th Edition):

Kuga, Hélio Koiti. “Estimação adaptativa de órbitas aplicada a satélites a baixa altitude.” 1981. Web. 31 Oct 2020.

Vancouver:

Kuga HK. Estimação adaptativa de órbitas aplicada a satélites a baixa altitude. [Internet] [Thesis]. Instituto Nacional de Pesquisas Espaciais; 1981. [cited 2020 Oct 31]. Available from: http://urlib.net/sid.inpe.br/[email protected]/2005/07.27.13.52.

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

Council of Science Editors:

Kuga HK. Estimação adaptativa de órbitas aplicada a satélites a baixa altitude. [Thesis]. Instituto Nacional de Pesquisas Espaciais; 1981. Available from: http://urlib.net/sid.inpe.br/[email protected]/2005/07.27.13.52

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

18. Kelly, Patrick W. Control of Geostationary Satellite Orbits Using Solar Radiation Pressure.

Degree: MS, Aerospace Engineering - Mechanical and Aerospace Engineering, 2016, University of Florida

 Solar radiation pressure (SRP) is the largest non-gravitational perturbation at geostationary orbit (GEO). Through deliberate changes in a satellite's orientation throughout orbit, the magnitudes of… (more)

Subjects/Keywords: Acceleration; Artificial satellites; Coordinate systems; Orbital eccentricity; Orbits; Sails; Simulations; Solar radiation; Sun; Velocity; control  – geostationary  – pressure  – radiation  – satellite  – solar

…Master of Science CONTROL OF GEOSTATIONARY SATELLITE ORBITS USING SOLAR RADIATION PRESSURE By… …propulsion. These orientations can be used to create new orbits for a satellite, without the use of… …this work presents methods for attaining desired satellite orbits for application with near… …component in i direction  Force vector 8 J Cost function m Satellite mass k… …Solar radiation pressure  Gravitational potential function r Satellite position vector… 

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

APA (6th Edition):

Kelly, P. W. (2016). Control of Geostationary Satellite Orbits Using Solar Radiation Pressure. (Masters Thesis). University of Florida. Retrieved from https://ufdc.ufl.edu/UFE0050077

Chicago Manual of Style (16th Edition):

Kelly, Patrick W. “Control of Geostationary Satellite Orbits Using Solar Radiation Pressure.” 2016. Masters Thesis, University of Florida. Accessed October 31, 2020. https://ufdc.ufl.edu/UFE0050077.

MLA Handbook (7th Edition):

Kelly, Patrick W. “Control of Geostationary Satellite Orbits Using Solar Radiation Pressure.” 2016. Web. 31 Oct 2020.

Vancouver:

Kelly PW. Control of Geostationary Satellite Orbits Using Solar Radiation Pressure. [Internet] [Masters thesis]. University of Florida; 2016. [cited 2020 Oct 31]. Available from: https://ufdc.ufl.edu/UFE0050077.

Council of Science Editors:

Kelly PW. Control of Geostationary Satellite Orbits Using Solar Radiation Pressure. [Masters Thesis]. University of Florida; 2016. Available from: https://ufdc.ufl.edu/UFE0050077

19. Roberto Luiz Galski. Desenvolvimento de um navegador autônomo, usando GPS, aplicado ao controle autônomo de órbita.

Degree: 2001, Instituto Nacional de Pesquisas Espaciais

The appearance of modern global positioning systems motivated the study and development of precise and robust systems for autonomous orbit determination of artificial satellites. These… (more)

Subjects/Keywords: ENGENHARIA E TECNOLOGIA ESPACIAL; Navegação autônoma; Determinação de orbita; Navegação espacial; Órbita baixa terrestre; Autonomous navigation; Orbit determination; Solar orbits; Satellite guidance; Low earth orbits; CBERS; Controle automático de vôo; Orientação de satélite; Órbitas heliosíncronas; Sistema de posicionamento global; ENGINEERING AND SPACE TECHNOLOGY; Automatic fligh control; Space navigation; Global positioning system

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

APA (6th Edition):

Galski, R. L. (2001). Desenvolvimento de um navegador autônomo, usando GPS, aplicado ao controle autônomo de órbita. (Thesis). Instituto Nacional de Pesquisas Espaciais. Retrieved from http://urlib.net/sid.inpe.br/jeferson/2004/09.01.11.28

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):

Galski, Roberto Luiz. “Desenvolvimento de um navegador autônomo, usando GPS, aplicado ao controle autônomo de órbita.” 2001. Thesis, Instituto Nacional de Pesquisas Espaciais. Accessed October 31, 2020. http://urlib.net/sid.inpe.br/jeferson/2004/09.01.11.28.

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

MLA Handbook (7th Edition):

Galski, Roberto Luiz. “Desenvolvimento de um navegador autônomo, usando GPS, aplicado ao controle autônomo de órbita.” 2001. Web. 31 Oct 2020.

Vancouver:

Galski RL. Desenvolvimento de um navegador autônomo, usando GPS, aplicado ao controle autônomo de órbita. [Internet] [Thesis]. Instituto Nacional de Pesquisas Espaciais; 2001. [cited 2020 Oct 31]. Available from: http://urlib.net/sid.inpe.br/jeferson/2004/09.01.11.28.

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

Council of Science Editors:

Galski RL. Desenvolvimento de um navegador autônomo, usando GPS, aplicado ao controle autônomo de órbita. [Thesis]. Instituto Nacional de Pesquisas Espaciais; 2001. Available from: http://urlib.net/sid.inpe.br/jeferson/2004/09.01.11.28

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

20. Paulo Marcelo Tasinaffo. Estruturas de integração neural Feedforward testadas em problemas de controle preditivo.

Degree: 2003, Instituto Nacional de Pesquisas Espaciais

This work presents, develops and tests a methodology for the modeling of dynamical systems applied to a scheme of predictive control. Feedforward neural networks are… (more)

Subjects/Keywords: integração numérica; cálculo diferencial; sistemas de controle preditivo; controle de atitude de satélites; transferência de órbitas; neural networks; dynamical systems; back propagation; satellite attitude control; transfer orbits; sistemas dinâmicos; derivadas médias; derivadas instantâneas; filtros de Kalman; nonlinear systems; numerical integration; differential calculus; Redes neurais; sistemas não-lineares; Kalman filters; predictive control systems

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

APA (6th Edition):

Tasinaffo, P. M. (2003). Estruturas de integração neural Feedforward testadas em problemas de controle preditivo. (Thesis). Instituto Nacional de Pesquisas Espaciais. Retrieved from http://urlib.net/sid.inpe.br/jeferson/2004/02.18.14.07

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):

Tasinaffo, Paulo Marcelo. “Estruturas de integração neural Feedforward testadas em problemas de controle preditivo.” 2003. Thesis, Instituto Nacional de Pesquisas Espaciais. Accessed October 31, 2020. http://urlib.net/sid.inpe.br/jeferson/2004/02.18.14.07.

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

MLA Handbook (7th Edition):

Tasinaffo, Paulo Marcelo. “Estruturas de integração neural Feedforward testadas em problemas de controle preditivo.” 2003. Web. 31 Oct 2020.

Vancouver:

Tasinaffo PM. Estruturas de integração neural Feedforward testadas em problemas de controle preditivo. [Internet] [Thesis]. Instituto Nacional de Pesquisas Espaciais; 2003. [cited 2020 Oct 31]. Available from: http://urlib.net/sid.inpe.br/jeferson/2004/02.18.14.07.

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

Council of Science Editors:

Tasinaffo PM. Estruturas de integração neural Feedforward testadas em problemas de controle preditivo. [Thesis]. Instituto Nacional de Pesquisas Espaciais; 2003. Available from: http://urlib.net/sid.inpe.br/jeferson/2004/02.18.14.07

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

21. Dutta, Atri. Optimal cooperative and non-cooperative peer-to-peer maneuvers for refueling satellites in circular constellations.

Degree: PhD, Aerospace Engineering, 2009, Georgia Tech

 On-orbit servicing (OOS) of space systems provides immense benefits by extending their lifetime, by reducing overall cost of space operations, and by adding flexibility to… (more)

Subjects/Keywords: Constellation graphs; Three-index assignment problem; NP-hardness; Network flows; Cooperative rendezvous; On-orbit servicing; Satellite refueling; Peer-to-peer refueling; Lambert's problem; Hohmann transfers; Phasing maneuvers; Artificial satellites Refueling; Artificial satellites Orbits; Artificial satellites Maintenance and repair; Mathematical optimization

…100 4.5 4.6 Peer-to-Peer Refueling Between Satellites in Different Orbits . . . . 105 4.7… …for Second Step of Mixed Refueling Strategy. Twelve Satellite Constellation… …deficient satellite, one of them performs an orbital transfer to rendezvous with the other… …flexibility to space-based programs. Naturally, the areas of formation flight and satellite clusters… …also assume the following information is available for each satellite: mass, initial position… 

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

APA (6th Edition):

Dutta, A. (2009). Optimal cooperative and non-cooperative peer-to-peer maneuvers for refueling satellites in circular constellations. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/28082

Chicago Manual of Style (16th Edition):

Dutta, Atri. “Optimal cooperative and non-cooperative peer-to-peer maneuvers for refueling satellites in circular constellations.” 2009. Doctoral Dissertation, Georgia Tech. Accessed October 31, 2020. http://hdl.handle.net/1853/28082.

MLA Handbook (7th Edition):

Dutta, Atri. “Optimal cooperative and non-cooperative peer-to-peer maneuvers for refueling satellites in circular constellations.” 2009. Web. 31 Oct 2020.

Vancouver:

Dutta A. Optimal cooperative and non-cooperative peer-to-peer maneuvers for refueling satellites in circular constellations. [Internet] [Doctoral dissertation]. Georgia Tech; 2009. [cited 2020 Oct 31]. Available from: http://hdl.handle.net/1853/28082.

Council of Science Editors:

Dutta A. Optimal cooperative and non-cooperative peer-to-peer maneuvers for refueling satellites in circular constellations. [Doctoral Dissertation]. Georgia Tech; 2009. Available from: http://hdl.handle.net/1853/28082

.