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University of Colorado

1. Handzo, Ryan E. Satellite Navigation Using High Definition Television Signals.

Degree: MS, 2016, University of Colorado

URL: https://scholar.colorado.edu/asen_gradetds/189

► Spacecraft operators can use a variety of observables to perform orbit determination throughout a mission. Currently the mission design community has an interest in…
(more)

Subjects/Keywords: spacecraft navigation; satellites; HDTV; signals; Aerospace Engineering

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APA (6^{th} Edition):

Handzo, R. E. (2016). Satellite Navigation Using High Definition Television Signals. (Masters Thesis). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/189

Chicago Manual of Style (16^{th} Edition):

Handzo, Ryan E. “Satellite Navigation Using High Definition Television Signals.” 2016. Masters Thesis, University of Colorado. Accessed March 07, 2021. https://scholar.colorado.edu/asen_gradetds/189.

MLA Handbook (7^{th} Edition):

Handzo, Ryan E. “Satellite Navigation Using High Definition Television Signals.” 2016. Web. 07 Mar 2021.

Vancouver:

Handzo RE. Satellite Navigation Using High Definition Television Signals. [Internet] [Masters thesis]. University of Colorado; 2016. [cited 2021 Mar 07]. Available from: https://scholar.colorado.edu/asen_gradetds/189.

Council of Science Editors:

Handzo RE. Satellite Navigation Using High Definition Television Signals. [Masters Thesis]. University of Colorado; 2016. Available from: https://scholar.colorado.edu/asen_gradetds/189

University of Colorado

2. Bezrouk, Collin J. Ballistic Capture into Lunar and Martian Distant Retrograde Orbits.

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

URL: https://scholar.colorado.edu/asen_gradetds/147

► Distant retrograde orbits (DROs) are a neutrally stable class of three-body orbits. Because of their stability, DROs cannot be targeted with a low-energy transfer…
(more)

Subjects/Keywords: ballistic capture; distant retrograde orbit; low-energy; mission design; Phobos; weak stability boundary; Aerospace Engineering

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APA (6^{th} Edition):

Bezrouk, C. J. (2016). Ballistic Capture into Lunar and Martian Distant Retrograde Orbits. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/147

Chicago Manual of Style (16^{th} Edition):

Bezrouk, Collin J. “Ballistic Capture into Lunar and Martian Distant Retrograde Orbits.” 2016. Doctoral Dissertation, University of Colorado. Accessed March 07, 2021. https://scholar.colorado.edu/asen_gradetds/147.

MLA Handbook (7^{th} Edition):

Bezrouk, Collin J. “Ballistic Capture into Lunar and Martian Distant Retrograde Orbits.” 2016. Web. 07 Mar 2021.

Vancouver:

Bezrouk CJ. Ballistic Capture into Lunar and Martian Distant Retrograde Orbits. [Internet] [Doctoral dissertation]. University of Colorado; 2016. [cited 2021 Mar 07]. Available from: https://scholar.colorado.edu/asen_gradetds/147.

Council of Science Editors:

Bezrouk CJ. Ballistic Capture into Lunar and Martian Distant Retrograde Orbits. [Doctoral Dissertation]. University of Colorado; 2016. Available from: https://scholar.colorado.edu/asen_gradetds/147

University of Colorado

3. Aziz, Jonathan David. Low-Thrust Many-Revolution Trajectory Optimization.

Degree: PhD, 2018, University of Colorado

URL: https://scholar.colorado.edu/asen_gradetds/210

► This dissertation presents a method for optimizing the trajectories of spacecraft that use low-thrust propulsion to maneuver through high counts of orbital revolutions. The…
(more)

Subjects/Keywords: differential dynamic programming; low-thrust propulsion; solar electric propulsion; spaceflight; sundman transformation; trajectory optimization; Aerospace Engineering; Models and Methods

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

APA (6^{th} Edition):

Aziz, J. D. (2018). Low-Thrust Many-Revolution Trajectory Optimization. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/210

Chicago Manual of Style (16^{th} Edition):

Aziz, Jonathan David. “Low-Thrust Many-Revolution Trajectory Optimization.” 2018. Doctoral Dissertation, University of Colorado. Accessed March 07, 2021. https://scholar.colorado.edu/asen_gradetds/210.

MLA Handbook (7^{th} Edition):

Aziz, Jonathan David. “Low-Thrust Many-Revolution Trajectory Optimization.” 2018. Web. 07 Mar 2021.

Vancouver:

Aziz JD. Low-Thrust Many-Revolution Trajectory Optimization. [Internet] [Doctoral dissertation]. University of Colorado; 2018. [cited 2021 Mar 07]. Available from: https://scholar.colorado.edu/asen_gradetds/210.

Council of Science Editors:

Aziz JD. Low-Thrust Many-Revolution Trajectory Optimization. [Doctoral Dissertation]. University of Colorado; 2018. Available from: https://scholar.colorado.edu/asen_gradetds/210

University of Colorado

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

Degree: PhD, 2018, University of Colorado

URL: https://scholar.colorado.edu/asen_gradetds/235

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

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

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APA (6^{th} Edition):

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

Chicago Manual of Style (16^{th} Edition):

De Smet, Stijn. “On the Design of Solar Gravity Driven Planetocentric Transfers Using Artificial Neural Networks.” 2018. Doctoral Dissertation, University of Colorado. Accessed March 07, 2021. https://scholar.colorado.edu/asen_gradetds/235.

MLA Handbook (7^{th} Edition):

De Smet, Stijn. “On the Design of Solar Gravity Driven Planetocentric Transfers Using Artificial Neural Networks.” 2018. Web. 07 Mar 2021.

Vancouver:

De Smet S. On the Design of Solar Gravity Driven Planetocentric Transfers Using Artificial Neural Networks. [Internet] [Doctoral dissertation]. University of Colorado; 2018. [cited 2021 Mar 07]. Available from: https://scholar.colorado.edu/asen_gradetds/235.

Council of Science Editors:

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

University of Colorado

5. Hesar, Siamak Ghanizadeh. A Framework for Precise Orbit Determination of Small Body Orbiting Spacecraft.

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

URL: https://scholar.colorado.edu/asen_gradetds/141

► Spacecraft flying in close proximity of small bodies face a very complex dynamical environment with numerous types of perturbing forces acting on them. Development…
(more)

Subjects/Keywords: Interior Gravity Field; Precise Orbit Determination; Small Body Navigation; Solar Radiation Pressure; Spacecraft Navigation; Thermal Radiation Pressure; Aerospace Engineering

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

APA (6^{th} Edition):

Hesar, S. G. (2016). A Framework for Precise Orbit Determination of Small Body Orbiting Spacecraft. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/141

Chicago Manual of Style (16^{th} Edition):

Hesar, Siamak Ghanizadeh. “A Framework for Precise Orbit Determination of Small Body Orbiting Spacecraft.” 2016. Doctoral Dissertation, University of Colorado. Accessed March 07, 2021. https://scholar.colorado.edu/asen_gradetds/141.

MLA Handbook (7^{th} Edition):

Hesar, Siamak Ghanizadeh. “A Framework for Precise Orbit Determination of Small Body Orbiting Spacecraft.” 2016. Web. 07 Mar 2021.

Vancouver:

Hesar SG. A Framework for Precise Orbit Determination of Small Body Orbiting Spacecraft. [Internet] [Doctoral dissertation]. University of Colorado; 2016. [cited 2021 Mar 07]. Available from: https://scholar.colorado.edu/asen_gradetds/141.

Council of Science Editors:

Hesar SG. A Framework for Precise Orbit Determination of Small Body Orbiting Spacecraft. [Doctoral Dissertation]. University of Colorado; 2016. Available from: https://scholar.colorado.edu/asen_gradetds/141

University of Colorado

6. Olikara, Zubin Philip. Computation of Quasi-Periodic Tori and Heteroclinic Connections in Astrodynamics Using Collocation Techniques.

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

URL: https://scholar.colorado.edu/asen_gradetds/144

► Many astrodynamical systems exhibit both ordered and chaotic motion. The invariant manifold structure organizes these behaviors and is a valuable tool for the design of…
(more)

Subjects/Keywords: Gauss-Legendre collocation; heteroclinic connections; invariant manifolds; quasi-periodic orbits; restricted 3-body problem; spacecraft trajectory design; Aerospace Engineering; Applied Mathematics

Record Details Similar Records

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

APA (6^{th} Edition):

Olikara, Z. P. (2016). Computation of Quasi-Periodic Tori and Heteroclinic Connections in Astrodynamics Using Collocation Techniques. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/144

Chicago Manual of Style (16^{th} Edition):

Olikara, Zubin Philip. “Computation of Quasi-Periodic Tori and Heteroclinic Connections in Astrodynamics Using Collocation Techniques.” 2016. Doctoral Dissertation, University of Colorado. Accessed March 07, 2021. https://scholar.colorado.edu/asen_gradetds/144.

MLA Handbook (7^{th} Edition):

Olikara, Zubin Philip. “Computation of Quasi-Periodic Tori and Heteroclinic Connections in Astrodynamics Using Collocation Techniques.” 2016. Web. 07 Mar 2021.

Vancouver:

Olikara ZP. Computation of Quasi-Periodic Tori and Heteroclinic Connections in Astrodynamics Using Collocation Techniques. [Internet] [Doctoral dissertation]. University of Colorado; 2016. [cited 2021 Mar 07]. Available from: https://scholar.colorado.edu/asen_gradetds/144.

Council of Science Editors:

Olikara ZP. Computation of Quasi-Periodic Tori and Heteroclinic Connections in Astrodynamics Using Collocation Techniques. [Doctoral Dissertation]. University of Colorado; 2016. Available from: https://scholar.colorado.edu/asen_gradetds/144

University of Colorado

7. Parrish, Nathan Luis Olin. Low Thrust Trajectory Optimization in Cislunar and Translunar Space.

Degree: PhD, 2018, University of Colorado

URL: https://scholar.colorado.edu/asen_gradetds/202

► Low-thrust propulsion technologies such as electric propulsion and solar sails are key to enabling many space missions which would be impractical with chemical propulsion.…
(more)

Subjects/Keywords: artificial intelligence; crtbp; electric propulsion; neural networks; optimization; Aerospace Engineering; Engineering

Record Details Similar Records

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

APA (6^{th} Edition):

Parrish, N. L. O. (2018). Low Thrust Trajectory Optimization in Cislunar and Translunar Space. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/202

Chicago Manual of Style (16^{th} Edition):

Parrish, Nathan Luis Olin. “Low Thrust Trajectory Optimization in Cislunar and Translunar Space.” 2018. Doctoral Dissertation, University of Colorado. Accessed March 07, 2021. https://scholar.colorado.edu/asen_gradetds/202.

MLA Handbook (7^{th} Edition):

Parrish, Nathan Luis Olin. “Low Thrust Trajectory Optimization in Cislunar and Translunar Space.” 2018. Web. 07 Mar 2021.

Vancouver:

Parrish NLO. Low Thrust Trajectory Optimization in Cislunar and Translunar Space. [Internet] [Doctoral dissertation]. University of Colorado; 2018. [cited 2021 Mar 07]. Available from: https://scholar.colorado.edu/asen_gradetds/202.

Council of Science Editors:

Parrish NLO. Low Thrust Trajectory Optimization in Cislunar and Translunar Space. [Doctoral Dissertation]. University of Colorado; 2018. Available from: https://scholar.colorado.edu/asen_gradetds/202

University of Colorado

8. 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

URL: https://scholar.colorado.edu/asen_gradetds/84

► 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 Details Similar Records

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

APA (6^{th} 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 (16^{th} Edition):

Lathrop, Brian Wesley. “An Investigation of Alternate Transfer Strategies to the Sun-Earth Triangular Lagrangian Points.” 2014. Doctoral Dissertation, University of Colorado. Accessed March 07, 2021. https://scholar.colorado.edu/asen_gradetds/84.

MLA Handbook (7^{th} Edition):

Lathrop, Brian Wesley. “An Investigation of Alternate Transfer Strategies to the Sun-Earth Triangular Lagrangian Points.” 2014. Web. 07 Mar 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 Mar 07]. 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

University of Colorado

9. Leonard, Jason Michael. Supporting Crewed Missions using LiAISON Navigation in the Earth-Moon System.

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

URL: https://scholar.colorado.edu/asen_gradetds/97

► Crewed navigation in certain regions of the Earth-Moon system provides a unique challenge due to the unstable dynamics and observation geometry relative to standard…
(more)

Subjects/Keywords: Autonomous Navigation; Navigation; Orbit Determination; Stochastic Processes; Navigation, Guidance, Control and Dynamics; Space Vehicles

Record Details Similar Records

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

APA (6^{th} Edition):

Leonard, J. M. (2015). Supporting Crewed Missions using LiAISON Navigation in the Earth-Moon System. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/97

Chicago Manual of Style (16^{th} Edition):

Leonard, Jason Michael. “Supporting Crewed Missions using LiAISON Navigation in the Earth-Moon System.” 2015. Doctoral Dissertation, University of Colorado. Accessed March 07, 2021. https://scholar.colorado.edu/asen_gradetds/97.

MLA Handbook (7^{th} Edition):

Leonard, Jason Michael. “Supporting Crewed Missions using LiAISON Navigation in the Earth-Moon System.” 2015. Web. 07 Mar 2021.

Vancouver:

Leonard JM. Supporting Crewed Missions using LiAISON Navigation in the Earth-Moon System. [Internet] [Doctoral dissertation]. University of Colorado; 2015. [cited 2021 Mar 07]. Available from: https://scholar.colorado.edu/asen_gradetds/97.

Council of Science Editors:

Leonard JM. Supporting Crewed Missions using LiAISON Navigation in the Earth-Moon System. [Doctoral Dissertation]. University of Colorado; 2015. Available from: https://scholar.colorado.edu/asen_gradetds/97

University of Colorado

10. Herman, Jonathan F.C. Improved Collocation Methods to Optimize Low-Thrust, Low-Energy Transfers in the Earth-Moon System.

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

URL: https://scholar.colorado.edu/asen_gradetds/116

► Modern and near-future Solar Electric Propulsion capabilities enable many new missions that were inconceivable using chemical propulsion systems. Many of these involve highly complex…
(more)

Subjects/Keywords: Astrodynamics; Electric Propulsion; Low-Thrust Propulsion; Parallel computing; Trajectory Optimization; Aerospace Engineering

Record Details Similar Records

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

APA (6^{th} Edition):

Herman, J. F. C. (2015). Improved Collocation Methods to Optimize Low-Thrust, Low-Energy Transfers in the Earth-Moon System. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/116

Chicago Manual of Style (16^{th} Edition):

Herman, Jonathan F C. “Improved Collocation Methods to Optimize Low-Thrust, Low-Energy Transfers in the Earth-Moon System.” 2015. Doctoral Dissertation, University of Colorado. Accessed March 07, 2021. https://scholar.colorado.edu/asen_gradetds/116.

MLA Handbook (7^{th} Edition):

Herman, Jonathan F C. “Improved Collocation Methods to Optimize Low-Thrust, Low-Energy Transfers in the Earth-Moon System.” 2015. Web. 07 Mar 2021.

Vancouver:

Herman JFC. Improved Collocation Methods to Optimize Low-Thrust, Low-Energy Transfers in the Earth-Moon System. [Internet] [Doctoral dissertation]. University of Colorado; 2015. [cited 2021 Mar 07]. Available from: https://scholar.colorado.edu/asen_gradetds/116.

Council of Science Editors:

Herman JFC. Improved Collocation Methods to Optimize Low-Thrust, Low-Energy Transfers in the Earth-Moon System. [Doctoral Dissertation]. University of Colorado; 2015. Available from: https://scholar.colorado.edu/asen_gradetds/116

University of Colorado

11. Ko, Hyun Chul. Representation of Unknown and Unmodeled Space Events for Satellites : Characteristics and Applications.

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

URL: https://scholar.colorado.edu/asen_gradetds/120

► A new way of representing unknown and unmodeled space events (USEs) with Thrust-Fourier-Coefficients (TFCs) is introduced and its applications to satellite orbit determination (OD)…
(more)

Subjects/Keywords: Event Detection; Event Representation; Maneuvering Satellite Tracking; Orbit Determination; Thrust-Fourier-Coefficients; Unknown Space Event; Mechanical Engineering; Navigation, Guidance, Control and Dynamics; Space Vehicles; Systems Engineering

Record Details Similar Records

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

APA (6^{th} Edition):

Ko, H. C. (2015). Representation of Unknown and Unmodeled Space Events for Satellites : Characteristics and Applications. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/120

Chicago Manual of Style (16^{th} Edition):

Ko, Hyun Chul. “Representation of Unknown and Unmodeled Space Events for Satellites : Characteristics and Applications.” 2015. Doctoral Dissertation, University of Colorado. Accessed March 07, 2021. https://scholar.colorado.edu/asen_gradetds/120.

MLA Handbook (7^{th} Edition):

Ko, Hyun Chul. “Representation of Unknown and Unmodeled Space Events for Satellites : Characteristics and Applications.” 2015. Web. 07 Mar 2021.

Vancouver:

Ko HC. Representation of Unknown and Unmodeled Space Events for Satellites : Characteristics and Applications. [Internet] [Doctoral dissertation]. University of Colorado; 2015. [cited 2021 Mar 07]. Available from: https://scholar.colorado.edu/asen_gradetds/120.

Council of Science Editors:

Ko HC. Representation of Unknown and Unmodeled Space Events for Satellites : Characteristics and Applications. [Doctoral Dissertation]. University of Colorado; 2015. Available from: https://scholar.colorado.edu/asen_gradetds/120