Advanced search options

Advanced Search Options 🞨

Browse by author name (“Author name starts with…”).

Find ETDs with:

in
/  
in
/  
in
/  
in

Written in Published in Earliest date Latest date

Sorted by

Results per page:

Sorted by: relevance · author · university · dateNew search

You searched for +publisher:"University of Colorado" +contributor:("Brandon Jones"). Showing records 1 – 12 of 12 total matches.

Search Limiters

Last 2 Years | English Only

No search limiters apply to these results.

▼ Search Limiters


University of Colorado

1. Anderson, Paul V. Characterizing Longitude-Dependent Orbital Debris Congestion in the Geosynchronous Orbit Regime.

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

  The geosynchronous orbit (GEO) is a unique commodity of the satellite industry that is becoming increasingly contaminated with orbital debris, but is heavily populated… (more)

Subjects/Keywords: active debris removal; geostationary orbit; geosynchronous orbit; orbital debris; Aerospace Engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Anderson, P. V. (2010). Characterizing Longitude-Dependent Orbital Debris Congestion in the Geosynchronous Orbit Regime. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/14

Chicago Manual of Style (16th Edition):

Anderson, Paul V. “Characterizing Longitude-Dependent Orbital Debris Congestion in the Geosynchronous Orbit Regime.” 2010. Doctoral Dissertation, University of Colorado. Accessed January 19, 2021. https://scholar.colorado.edu/asen_gradetds/14.

MLA Handbook (7th Edition):

Anderson, Paul V. “Characterizing Longitude-Dependent Orbital Debris Congestion in the Geosynchronous Orbit Regime.” 2010. Web. 19 Jan 2021.

Vancouver:

Anderson PV. Characterizing Longitude-Dependent Orbital Debris Congestion in the Geosynchronous Orbit Regime. [Internet] [Doctoral dissertation]. University of Colorado; 2010. [cited 2021 Jan 19]. Available from: https://scholar.colorado.edu/asen_gradetds/14.

Council of Science Editors:

Anderson PV. Characterizing Longitude-Dependent Orbital Debris Congestion in the Geosynchronous Orbit Regime. [Doctoral Dissertation]. University of Colorado; 2010. Available from: https://scholar.colorado.edu/asen_gradetds/14


University of Colorado

2. Trowbridge, Michael Aaron. Autonomous 3D Model Generation of Orbital Debris using Point Cloud Sensors.

Degree: MS, Aerospace Engineering Sciences, 2014, University of Colorado

  A software prototype for autonomous 3D scanning of uncooperatively rotating orbital debris using a point cloud sensor is designed and tested. The software successfully… (more)

Subjects/Keywords: 3D scanning; explicit loop closure heuristic; Graph SLAM; model generation; orbital debris; point clouds; Aerospace Engineering; Artificial Intelligence and Robotics; Computer-Aided Engineering and Design; Systems Engineering and Multidisciplinary Design Optimization

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Trowbridge, M. A. (2014). Autonomous 3D Model Generation of Orbital Debris using Point Cloud Sensors. (Masters Thesis). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/86

Chicago Manual of Style (16th Edition):

Trowbridge, Michael Aaron. “Autonomous 3D Model Generation of Orbital Debris using Point Cloud Sensors.” 2014. Masters Thesis, University of Colorado. Accessed January 19, 2021. https://scholar.colorado.edu/asen_gradetds/86.

MLA Handbook (7th Edition):

Trowbridge, Michael Aaron. “Autonomous 3D Model Generation of Orbital Debris using Point Cloud Sensors.” 2014. Web. 19 Jan 2021.

Vancouver:

Trowbridge MA. Autonomous 3D Model Generation of Orbital Debris using Point Cloud Sensors. [Internet] [Masters thesis]. University of Colorado; 2014. [cited 2021 Jan 19]. Available from: https://scholar.colorado.edu/asen_gradetds/86.

Council of Science Editors:

Trowbridge MA. Autonomous 3D Model Generation of Orbital Debris using Point Cloud Sensors. [Masters Thesis]. University of Colorado; 2014. Available from: https://scholar.colorado.edu/asen_gradetds/86


University of Colorado

3. Chabot, Joshua A. A Spherical Magnetic Dipole Actuator for Spacecraft Attitude Control.

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

  Spacecraft generally require multiple attitude control devices to achieve full attitude actuation because of the limited control authority a single, traditional device can provide.… (more)

Subjects/Keywords: attitude control; magetic dipole; magnetic bearing; reaction sphere; spherical actuator; Navigation, Guidance, Control and Dynamics; Space Vehicles

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Chabot, J. A. (2015). A Spherical Magnetic Dipole Actuator for Spacecraft Attitude Control. (Masters Thesis). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/100

Chicago Manual of Style (16th Edition):

Chabot, Joshua A. “A Spherical Magnetic Dipole Actuator for Spacecraft Attitude Control.” 2015. Masters Thesis, University of Colorado. Accessed January 19, 2021. https://scholar.colorado.edu/asen_gradetds/100.

MLA Handbook (7th Edition):

Chabot, Joshua A. “A Spherical Magnetic Dipole Actuator for Spacecraft Attitude Control.” 2015. Web. 19 Jan 2021.

Vancouver:

Chabot JA. A Spherical Magnetic Dipole Actuator for Spacecraft Attitude Control. [Internet] [Masters thesis]. University of Colorado; 2015. [cited 2021 Jan 19]. Available from: https://scholar.colorado.edu/asen_gradetds/100.

Council of Science Editors:

Chabot JA. A Spherical Magnetic Dipole Actuator for Spacecraft Attitude Control. [Masters Thesis]. University of Colorado; 2015. Available from: https://scholar.colorado.edu/asen_gradetds/100


University of Colorado

4. Jasper, Lee E.Z. Open-Loop Thrust Profile Development for Tethered Towing of Large Space Objects.

Degree: PhD, Aerospace Engineering Sciences, 2014, University of Colorado

  Towing objects in space has become an increasingly researched mission concept. Active debris removal, satellite servicing, and asteroid retrieval concepts in many cases rely… (more)

Subjects/Keywords: active debris removal; input shaping; orbital debris; space tether; tethered towing; Aerospace Engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Jasper, L. E. Z. (2014). Open-Loop Thrust Profile Development for Tethered Towing of Large Space Objects. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/82

Chicago Manual of Style (16th Edition):

Jasper, Lee E Z. “Open-Loop Thrust Profile Development for Tethered Towing of Large Space Objects.” 2014. Doctoral Dissertation, University of Colorado. Accessed January 19, 2021. https://scholar.colorado.edu/asen_gradetds/82.

MLA Handbook (7th Edition):

Jasper, Lee E Z. “Open-Loop Thrust Profile Development for Tethered Towing of Large Space Objects.” 2014. Web. 19 Jan 2021.

Vancouver:

Jasper LEZ. Open-Loop Thrust Profile Development for Tethered Towing of Large Space Objects. [Internet] [Doctoral dissertation]. University of Colorado; 2014. [cited 2021 Jan 19]. Available from: https://scholar.colorado.edu/asen_gradetds/82.

Council of Science Editors:

Jasper LEZ. Open-Loop Thrust Profile Development for Tethered Towing of Large Space Objects. [Doctoral Dissertation]. University of Colorado; 2014. Available from: https://scholar.colorado.edu/asen_gradetds/82


University of Colorado

5. Hadigol, Mohammad. Uncertainty Quantification of Coupled Problems with Applications to Lithium-ion Batteries.

Degree: PhD, Aerospace Engineering Sciences, 2016, University of Colorado

  This thesis includes three main parts that are concerned with the propagation of uncertainty across high-dimensional coupled problems with applications to Lithium-ion batteries (LIBs).… (more)

Subjects/Keywords: Coupled Domain; High-dimensional; Lithium-ion Battery; Optimal Sampling; Polynomial Chaos Expansion; Uncertainty Quantification; Applied Mathematics; Engineering; Power and Energy

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Hadigol, M. (2016). Uncertainty Quantification of Coupled Problems with Applications to Lithium-ion Batteries. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/137

Chicago Manual of Style (16th Edition):

Hadigol, Mohammad. “Uncertainty Quantification of Coupled Problems with Applications to Lithium-ion Batteries.” 2016. Doctoral Dissertation, University of Colorado. Accessed January 19, 2021. https://scholar.colorado.edu/asen_gradetds/137.

MLA Handbook (7th Edition):

Hadigol, Mohammad. “Uncertainty Quantification of Coupled Problems with Applications to Lithium-ion Batteries.” 2016. Web. 19 Jan 2021.

Vancouver:

Hadigol M. Uncertainty Quantification of Coupled Problems with Applications to Lithium-ion Batteries. [Internet] [Doctoral dissertation]. University of Colorado; 2016. [cited 2021 Jan 19]. Available from: https://scholar.colorado.edu/asen_gradetds/137.

Council of Science Editors:

Hadigol M. Uncertainty Quantification of Coupled Problems with Applications to Lithium-ion Batteries. [Doctoral Dissertation]. University of Colorado; 2016. Available from: https://scholar.colorado.edu/asen_gradetds/137


University of Colorado

6. Gehly, Steven. Estimation of Geosynchronous Space Objects Using Finite Set Statistics Filtering Methods.

Degree: PhD, Aerospace Engineering Sciences, 2016, University of Colorado

 The use of near Earth space has increased dramatically in the past few decades, and operational satellites are an integral part of modern society. The… (more)

Subjects/Keywords: Geosynchronous Orbit; Information Gain; Initial Orbit Determination; Multitarget Filtering; Random Finite Sets; Sensor Allocation; Aerospace Engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Gehly, S. (2016). Estimation of Geosynchronous Space Objects Using Finite Set Statistics Filtering Methods. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/148

Chicago Manual of Style (16th Edition):

Gehly, Steven. “Estimation of Geosynchronous Space Objects Using Finite Set Statistics Filtering Methods.” 2016. Doctoral Dissertation, University of Colorado. Accessed January 19, 2021. https://scholar.colorado.edu/asen_gradetds/148.

MLA Handbook (7th Edition):

Gehly, Steven. “Estimation of Geosynchronous Space Objects Using Finite Set Statistics Filtering Methods.” 2016. Web. 19 Jan 2021.

Vancouver:

Gehly S. Estimation of Geosynchronous Space Objects Using Finite Set Statistics Filtering Methods. [Internet] [Doctoral dissertation]. University of Colorado; 2016. [cited 2021 Jan 19]. Available from: https://scholar.colorado.edu/asen_gradetds/148.

Council of Science Editors:

Gehly S. Estimation of Geosynchronous Space Objects Using Finite Set Statistics Filtering Methods. [Doctoral Dissertation]. University of Colorado; 2016. Available from: https://scholar.colorado.edu/asen_gradetds/148


University of Colorado

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

Degree: PhD, 2017, University of Colorado

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

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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Geeraert, Jeroen L. “Multi-Satellite Orbit Determination Using Interferometric Observables with RF Localization Applications.” 2017. Doctoral Dissertation, University of Colorado. Accessed January 19, 2021. https://scholar.colorado.edu/asen_gradetds/192.

MLA Handbook (7th Edition):

Geeraert, Jeroen L. “Multi-Satellite Orbit Determination Using Interferometric Observables with RF Localization Applications.” 2017. Web. 19 Jan 2021.

Vancouver:

Geeraert JL. Multi-Satellite Orbit Determination Using Interferometric Observables with RF Localization Applications. [Internet] [Doctoral dissertation]. University of Colorado; 2017. [cited 2021 Jan 19]. Available from: https://scholar.colorado.edu/asen_gradetds/192.

Council of Science Editors:

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


University of Colorado

8. Anderson, Paul Vincent. Characterizing Longitude-Dependent Orbital Debris Congestion in the Geosynchronous Orbit Regime.

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

  The geosynchronous orbit (GEO) is a unique commodity of the satellite industry that is becoming increasingly contaminated with orbital debris, but is heavily populated… (more)

Subjects/Keywords: active debris removal; geostationary orbit; geosynchronous orbit; orbital debris; Aerospace Engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Anderson, P. V. (2015). Characterizing Longitude-Dependent Orbital Debris Congestion in the Geosynchronous Orbit Regime. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/91

Chicago Manual of Style (16th Edition):

Anderson, Paul Vincent. “Characterizing Longitude-Dependent Orbital Debris Congestion in the Geosynchronous Orbit Regime.” 2015. Doctoral Dissertation, University of Colorado. Accessed January 19, 2021. https://scholar.colorado.edu/asen_gradetds/91.

MLA Handbook (7th Edition):

Anderson, Paul Vincent. “Characterizing Longitude-Dependent Orbital Debris Congestion in the Geosynchronous Orbit Regime.” 2015. Web. 19 Jan 2021.

Vancouver:

Anderson PV. Characterizing Longitude-Dependent Orbital Debris Congestion in the Geosynchronous Orbit Regime. [Internet] [Doctoral dissertation]. University of Colorado; 2015. [cited 2021 Jan 19]. Available from: https://scholar.colorado.edu/asen_gradetds/91.

Council of Science Editors:

Anderson PV. Characterizing Longitude-Dependent Orbital Debris Congestion in the Geosynchronous Orbit Regime. [Doctoral Dissertation]. University of Colorado; 2015. Available from: https://scholar.colorado.edu/asen_gradetds/91


University of Colorado

9. Stevenson, Daan. Remote Spacecraft Attitude Control by Coulomb Charging.

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

  The possibility of inter-spacecraft collisions is a serious concern at Geosynchronous altitudes, where many high-value assets operate in proximity to countless debris objects whose… (more)

Subjects/Keywords: electrostatic modeling; high voltage experimentation; spacecraft attitude control; spacecraft charging; Multi-Vehicle Systems and Air Traffic Control; Navigation, Guidance, Control and Dynamics; Space Vehicles

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Stevenson, D. (2015). Remote Spacecraft Attitude Control by Coulomb Charging. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/94

Chicago Manual of Style (16th Edition):

Stevenson, Daan. “Remote Spacecraft Attitude Control by Coulomb Charging.” 2015. Doctoral Dissertation, University of Colorado. Accessed January 19, 2021. https://scholar.colorado.edu/asen_gradetds/94.

MLA Handbook (7th Edition):

Stevenson, Daan. “Remote Spacecraft Attitude Control by Coulomb Charging.” 2015. Web. 19 Jan 2021.

Vancouver:

Stevenson D. Remote Spacecraft Attitude Control by Coulomb Charging. [Internet] [Doctoral dissertation]. University of Colorado; 2015. [cited 2021 Jan 19]. Available from: https://scholar.colorado.edu/asen_gradetds/94.

Council of Science Editors:

Stevenson D. Remote Spacecraft Attitude Control by Coulomb Charging. [Doctoral Dissertation]. University of Colorado; 2015. Available from: https://scholar.colorado.edu/asen_gradetds/94


University of Colorado

10. O'Keefe, Stephen Andrew. Autonomous Sun-Direction Estimation Using Partially Underdetermined Coarse Sun Sensor Configurations.

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

  In recent years there has been a significant increase in interest in smaller satellites as lower cost alternatives to traditional satellites, particularly with the… (more)

Subjects/Keywords: Coarse Sun Sensors; Sun-Direction Estimation; Underdetermined; CubeSat; small satellite; mission limitation; Multi-Vehicle Systems and Air Traffic Control; Systems Engineering and Multidisciplinary Design Optimization; The Sun and the Solar System

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

O'Keefe, S. A. (2015). Autonomous Sun-Direction Estimation Using Partially Underdetermined Coarse Sun Sensor Configurations. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/95

Chicago Manual of Style (16th Edition):

O'Keefe, Stephen Andrew. “Autonomous Sun-Direction Estimation Using Partially Underdetermined Coarse Sun Sensor Configurations.” 2015. Doctoral Dissertation, University of Colorado. Accessed January 19, 2021. https://scholar.colorado.edu/asen_gradetds/95.

MLA Handbook (7th Edition):

O'Keefe, Stephen Andrew. “Autonomous Sun-Direction Estimation Using Partially Underdetermined Coarse Sun Sensor Configurations.” 2015. Web. 19 Jan 2021.

Vancouver:

O'Keefe SA. Autonomous Sun-Direction Estimation Using Partially Underdetermined Coarse Sun Sensor Configurations. [Internet] [Doctoral dissertation]. University of Colorado; 2015. [cited 2021 Jan 19]. Available from: https://scholar.colorado.edu/asen_gradetds/95.

Council of Science Editors:

O'Keefe SA. Autonomous Sun-Direction Estimation Using Partially Underdetermined Coarse Sun Sensor Configurations. [Doctoral Dissertation]. University of Colorado; 2015. Available from: https://scholar.colorado.edu/asen_gradetds/95


University of Colorado

11. Peng, Ji. Uncertainty Quantification via Sparse Polynomial Chaos Expansion.

Degree: PhD, Mechanical Engineering, 2015, University of Colorado

  Uncertainty quantification (UQ) is an emerging research area that aims to develop methods for accurate predictions of quantities of interest (QoI's) from complex engineering… (more)

Subjects/Keywords: Basis design; Compressive sampling; Polynomial chaos expansion; Sparse approximation; Uncertainty quantification; Applied Mathematics; Mechanical Engineering; Statistics and Probability

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Peng, J. (2015). Uncertainty Quantification via Sparse Polynomial Chaos Expansion. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/mcen_gradetds/112

Chicago Manual of Style (16th Edition):

Peng, Ji. “Uncertainty Quantification via Sparse Polynomial Chaos Expansion.” 2015. Doctoral Dissertation, University of Colorado. Accessed January 19, 2021. https://scholar.colorado.edu/mcen_gradetds/112.

MLA Handbook (7th Edition):

Peng, Ji. “Uncertainty Quantification via Sparse Polynomial Chaos Expansion.” 2015. Web. 19 Jan 2021.

Vancouver:

Peng J. Uncertainty Quantification via Sparse Polynomial Chaos Expansion. [Internet] [Doctoral dissertation]. University of Colorado; 2015. [cited 2021 Jan 19]. Available from: https://scholar.colorado.edu/mcen_gradetds/112.

Council of Science Editors:

Peng J. Uncertainty Quantification via Sparse Polynomial Chaos Expansion. [Doctoral Dissertation]. University of Colorado; 2015. Available from: https://scholar.colorado.edu/mcen_gradetds/112


University of Colorado

12. Lathrop, Brian Wesley. An Investigation of Alternate Transfer Strategies to the Sun-Earth Triangular Lagrangian Points.

Degree: PhD, Aerospace Engineering Sciences, 2014, University of Colorado

  Techniques for low energy transfers have been applied to constructing trajectories to various locations in the solar system. Previous techniques have concentrated on orbit… (more)

Subjects/Keywords: invariant manifolds; L4 L5; Lagrangian points; Low Energy Transfer; periodic orbits; three-body dynamics; Astrodynamics; Navigation, Guidance, Control and Dynamics

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Lathrop, B. W. (2014). An Investigation of Alternate Transfer Strategies to the Sun-Earth Triangular Lagrangian Points. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/84

Chicago Manual of Style (16th Edition):

Lathrop, Brian Wesley. “An Investigation of Alternate Transfer Strategies to the Sun-Earth Triangular Lagrangian Points.” 2014. Doctoral Dissertation, University of Colorado. Accessed January 19, 2021. https://scholar.colorado.edu/asen_gradetds/84.

MLA Handbook (7th Edition):

Lathrop, Brian Wesley. “An Investigation of Alternate Transfer Strategies to the Sun-Earth Triangular Lagrangian Points.” 2014. Web. 19 Jan 2021.

Vancouver:

Lathrop BW. An Investigation of Alternate Transfer Strategies to the Sun-Earth Triangular Lagrangian Points. [Internet] [Doctoral dissertation]. University of Colorado; 2014. [cited 2021 Jan 19]. Available from: https://scholar.colorado.edu/asen_gradetds/84.

Council of Science Editors:

Lathrop BW. An Investigation of Alternate Transfer Strategies to the Sun-Earth Triangular Lagrangian Points. [Doctoral Dissertation]. University of Colorado; 2014. Available from: https://scholar.colorado.edu/asen_gradetds/84

.