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University of Colorado

1. Holzinger, Marcus J. Optimal Control Applications in Space Situational Awareness.

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

URL: http://scholar.colorado.edu/asen_gradetds/20

► There are currently more than 19,000 trackable objects in Earth orbit, 1,300 of which are active. With so many objects populating the space object…
(more)

Subjects/Keywords: Aerospace; Correlation; Optimal Control; Range; Reachability; Space Situational Awareness; Astrodynamics; Multi-Vehicle Systems and Air Traffic Control

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APA (6^{th} Edition):

Holzinger, M. J. (2011). Optimal Control Applications in Space Situational Awareness. (Doctoral Dissertation). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/20

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

Holzinger, Marcus J. “Optimal Control Applications in Space Situational Awareness.” 2011. Doctoral Dissertation, University of Colorado. Accessed December 13, 2019. http://scholar.colorado.edu/asen_gradetds/20.

MLA Handbook (7^{th} Edition):

Holzinger, Marcus J. “Optimal Control Applications in Space Situational Awareness.” 2011. Web. 13 Dec 2019.

Vancouver:

Holzinger MJ. Optimal Control Applications in Space Situational Awareness. [Internet] [Doctoral dissertation]. University of Colorado; 2011. [cited 2019 Dec 13]. Available from: http://scholar.colorado.edu/asen_gradetds/20.

Council of Science Editors:

Holzinger MJ. Optimal Control Applications in Space Situational Awareness. [Doctoral Dissertation]. University of Colorado; 2011. Available from: http://scholar.colorado.edu/asen_gradetds/20

University of Colorado

2. Hirabayashi, Masatoshi. Structural Stability of Asteroids.

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

URL: http://scholar.colorado.edu/asen_gradetds/88

► This thesis develops a technique for analyzing the internal structure of an irregularly shaped asteroid. This research focuses on asteroid (216) Kleopatra, a few-hundred-kilometer-sized…
(more)

Subjects/Keywords: Asteroids; Deformation/Disruption; Dynamics; Structure; Astrophysics and Astronomy; Other Engineering; The Sun and the Solar System

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APA (6^{th} Edition):

Hirabayashi, M. (2014). Structural Stability of Asteroids. (Doctoral Dissertation). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/88

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

Hirabayashi, Masatoshi. “Structural Stability of Asteroids.” 2014. Doctoral Dissertation, University of Colorado. Accessed December 13, 2019. http://scholar.colorado.edu/asen_gradetds/88.

MLA Handbook (7^{th} Edition):

Hirabayashi, Masatoshi. “Structural Stability of Asteroids.” 2014. Web. 13 Dec 2019.

Vancouver:

Hirabayashi M. Structural Stability of Asteroids. [Internet] [Doctoral dissertation]. University of Colorado; 2014. [cited 2019 Dec 13]. Available from: http://scholar.colorado.edu/asen_gradetds/88.

Council of Science Editors:

Hirabayashi M. Structural Stability of Asteroids. [Doctoral Dissertation]. University of Colorado; 2014. Available from: http://scholar.colorado.edu/asen_gradetds/88

University of Colorado

3. 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

URL: https://scholar.colorado.edu/asen_gradetds/26

► 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 (6^{th} 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 (16^{th} Edition):

McMahon, Jay Warren. “An Analytical Theory for the Perturbative Effect of Solar Radiation Pressure on Natural and Artificial Satellites.” 2011. Doctoral Dissertation, University of Colorado. Accessed December 13, 2019. https://scholar.colorado.edu/asen_gradetds/26.

MLA Handbook (7^{th} Edition):

McMahon, Jay Warren. “An Analytical Theory for the Perturbative Effect of Solar Radiation Pressure on Natural and Artificial Satellites.” 2011. Web. 13 Dec 2019.

Vancouver:

McMahon JW. An Analytical Theory for the Perturbative Effect of Solar Radiation Pressure on Natural and Artificial Satellites. [Internet] [Doctoral dissertation]. University of Colorado; 2011. [cited 2019 Dec 13]. Available from: https://scholar.colorado.edu/asen_gradetds/26.

Council of Science Editors:

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

University of Colorado

4. Albuja, Antonella A. Rotational Dynamics of Inactive Satellites as a Result of the YORP Effect.

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

URL: http://scholar.colorado.edu/asen_gradetds/113

► Observations of inactive satellites in Earth orbit show that these objects are generally rotating, some with very fast rotation rates. In addition, observations indicate…
(more)

Subjects/Keywords: space debris; Co coefficient; GOES; Aerospace Engineering

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APA (6^{th} Edition):

Albuja, A. A. (2015). Rotational Dynamics of Inactive Satellites as a Result of the YORP Effect. (Doctoral Dissertation). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/113

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

Albuja, Antonella A. “Rotational Dynamics of Inactive Satellites as a Result of the YORP Effect.” 2015. Doctoral Dissertation, University of Colorado. Accessed December 13, 2019. http://scholar.colorado.edu/asen_gradetds/113.

MLA Handbook (7^{th} Edition):

Albuja, Antonella A. “Rotational Dynamics of Inactive Satellites as a Result of the YORP Effect.” 2015. Web. 13 Dec 2019.

Vancouver:

Albuja AA. Rotational Dynamics of Inactive Satellites as a Result of the YORP Effect. [Internet] [Doctoral dissertation]. University of Colorado; 2015. [cited 2019 Dec 13]. Available from: http://scholar.colorado.edu/asen_gradetds/113.

Council of Science Editors:

Albuja AA. Rotational Dynamics of Inactive Satellites as a Result of the YORP Effect. [Doctoral Dissertation]. University of Colorado; 2015. Available from: http://scholar.colorado.edu/asen_gradetds/113

University of Colorado

5. Lubey, Daniel Patrick. Maneuver Detection and Reconstruction in Data Sparse Systems with an Optimal Control Based Estimator.

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

URL: http://scholar.colorado.edu/asen_gradetds/114

► The Big Sky Theory once posited that the volume of Earth's orbital environment is so large that the chance of a collision ever occurring…
(more)

Subjects/Keywords: orbit determination; state estimation; OCBE; ballistic; smoother; Aerospace Engineering

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APA (6^{th} Edition):

Lubey, D. P. (2015). Maneuver Detection and Reconstruction in Data Sparse Systems with an Optimal Control Based Estimator. (Doctoral Dissertation). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/114

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

Lubey, Daniel Patrick. “Maneuver Detection and Reconstruction in Data Sparse Systems with an Optimal Control Based Estimator.” 2015. Doctoral Dissertation, University of Colorado. Accessed December 13, 2019. http://scholar.colorado.edu/asen_gradetds/114.

MLA Handbook (7^{th} Edition):

Lubey, Daniel Patrick. “Maneuver Detection and Reconstruction in Data Sparse Systems with an Optimal Control Based Estimator.” 2015. Web. 13 Dec 2019.

Vancouver:

Lubey DP. Maneuver Detection and Reconstruction in Data Sparse Systems with an Optimal Control Based Estimator. [Internet] [Doctoral dissertation]. University of Colorado; 2015. [cited 2019 Dec 13]. Available from: http://scholar.colorado.edu/asen_gradetds/114.

Council of Science Editors:

Lubey DP. Maneuver Detection and Reconstruction in Data Sparse Systems with an Optimal Control Based Estimator. [Doctoral Dissertation]. University of Colorado; 2015. Available from: http://scholar.colorado.edu/asen_gradetds/114

University of Colorado

6. Van wal, Stefaan. High-Fidelity Simulation of Small-Body Lander/Rover Spacecraft.

Degree: PhD, 2018, University of Colorado

URL: https://scholar.colorado.edu/asen_gradetds/200

► The scientific return of spacecraft missions that explore solar system small bodies can be increased through the inclusion of surface exploration with deployed probes.…
(more)

Subjects/Keywords: asteroid; comet; deployment; lander; rover; simulation; Aerospace Engineering; Models and Methods

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APA (6^{th} Edition):

Van wal, S. (2018). High-Fidelity Simulation of Small-Body Lander/Rover Spacecraft. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/200

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

Van wal, Stefaan. “High-Fidelity Simulation of Small-Body Lander/Rover Spacecraft.” 2018. Doctoral Dissertation, University of Colorado. Accessed December 13, 2019. https://scholar.colorado.edu/asen_gradetds/200.

MLA Handbook (7^{th} Edition):

Van wal, Stefaan. “High-Fidelity Simulation of Small-Body Lander/Rover Spacecraft.” 2018. Web. 13 Dec 2019.

Vancouver:

Van wal S. High-Fidelity Simulation of Small-Body Lander/Rover Spacecraft. [Internet] [Doctoral dissertation]. University of Colorado; 2018. [cited 2019 Dec 13]. Available from: https://scholar.colorado.edu/asen_gradetds/200.

Council of Science Editors:

Van wal S. High-Fidelity Simulation of Small-Body Lander/Rover Spacecraft. [Doctoral Dissertation]. University of Colorado; 2018. Available from: https://scholar.colorado.edu/asen_gradetds/200

University of Colorado

7. Jacobson, Seth Andrew. Dynamical evolution of small bodies in the Solar System.

Degree: PhD, Astrophysical & Planetary Sciences, 2012, University of Colorado

URL: http://scholar.colorado.edu/astr_gradetds/21

► This thesis explores the dynamical evolution of small bodies in the Solar System. It focuses on the asteroid population but parts of the theory…
(more)

Subjects/Keywords: Asteroid; Binary Asteroids; Dynamics; Astrophysics and Astronomy; Paleontology

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APA (6^{th} Edition):

Jacobson, S. A. (2012). Dynamical evolution of small bodies in the Solar System. (Doctoral Dissertation). University of Colorado. Retrieved from http://scholar.colorado.edu/astr_gradetds/21

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

Jacobson, Seth Andrew. “Dynamical evolution of small bodies in the Solar System.” 2012. Doctoral Dissertation, University of Colorado. Accessed December 13, 2019. http://scholar.colorado.edu/astr_gradetds/21.

MLA Handbook (7^{th} Edition):

Jacobson, Seth Andrew. “Dynamical evolution of small bodies in the Solar System.” 2012. Web. 13 Dec 2019.

Vancouver:

Jacobson SA. Dynamical evolution of small bodies in the Solar System. [Internet] [Doctoral dissertation]. University of Colorado; 2012. [cited 2019 Dec 13]. Available from: http://scholar.colorado.edu/astr_gradetds/21.

Council of Science Editors:

Jacobson SA. Dynamical evolution of small bodies in the Solar System. [Doctoral Dissertation]. University of Colorado; 2012. Available from: http://scholar.colorado.edu/astr_gradetds/21

University of Colorado

8. Fujimoto, Kohei. New Methods in Optical Track Association and Uncertainty Mapping of Earth-Orbiting Objects.

Degree: PhD, Aerospace Engineering Sciences, 2013, University of Colorado

URL: http://scholar.colorado.edu/asen_gradetds/57

► As more and more sensing capabilities for space surveillance are introduced, we expect that both correlated and uncorrelated tracks of resident space objects will…
(more)

Subjects/Keywords: admissible region; astrodynamics; optical observations; propagation of uncertainty; space situational awareness; too-short arc; Aerospace Engineering

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APA (6^{th} Edition):

Fujimoto, K. (2013). New Methods in Optical Track Association and Uncertainty Mapping of Earth-Orbiting Objects. (Doctoral Dissertation). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/57

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

Fujimoto, Kohei. “New Methods in Optical Track Association and Uncertainty Mapping of Earth-Orbiting Objects.” 2013. Doctoral Dissertation, University of Colorado. Accessed December 13, 2019. http://scholar.colorado.edu/asen_gradetds/57.

MLA Handbook (7^{th} Edition):

Fujimoto, Kohei. “New Methods in Optical Track Association and Uncertainty Mapping of Earth-Orbiting Objects.” 2013. Web. 13 Dec 2019.

Vancouver:

Fujimoto K. New Methods in Optical Track Association and Uncertainty Mapping of Earth-Orbiting Objects. [Internet] [Doctoral dissertation]. University of Colorado; 2013. [cited 2019 Dec 13]. Available from: http://scholar.colorado.edu/asen_gradetds/57.

Council of Science Editors:

Fujimoto K. New Methods in Optical Track Association and Uncertainty Mapping of Earth-Orbiting Objects. [Doctoral Dissertation]. University of Colorado; 2013. Available from: http://scholar.colorado.edu/asen_gradetds/57

University of Colorado

9. Boone, Dylan Robert. Integration of Geodesy Mission Design and Navigation for Planetary Satellite Orbiters.

Degree: PhD, Aerospace Engineering Sciences, 2013, University of Colorado

URL: http://scholar.colorado.edu/asen_gradetds/66

► Planetary satellites have become the primary targets of proposed missions to the outer planets as the places in the Solar System most likely to…
(more)

Subjects/Keywords: covariance; Enceladus; Europa; manifolds; periodic orbits; Aerospace Engineering

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APA (6^{th} Edition):

Boone, D. R. (2013). Integration of Geodesy Mission Design and Navigation for Planetary Satellite Orbiters. (Doctoral Dissertation). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/66

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

Boone, Dylan Robert. “Integration of Geodesy Mission Design and Navigation for Planetary Satellite Orbiters.” 2013. Doctoral Dissertation, University of Colorado. Accessed December 13, 2019. http://scholar.colorado.edu/asen_gradetds/66.

MLA Handbook (7^{th} Edition):

Boone, Dylan Robert. “Integration of Geodesy Mission Design and Navigation for Planetary Satellite Orbiters.” 2013. Web. 13 Dec 2019.

Vancouver:

Boone DR. Integration of Geodesy Mission Design and Navigation for Planetary Satellite Orbiters. [Internet] [Doctoral dissertation]. University of Colorado; 2013. [cited 2019 Dec 13]. Available from: http://scholar.colorado.edu/asen_gradetds/66.

Council of Science Editors:

Boone DR. Integration of Geodesy Mission Design and Navigation for Planetary Satellite Orbiters. [Doctoral Dissertation]. University of Colorado; 2013. Available from: http://scholar.colorado.edu/asen_gradetds/66

University of Colorado

10. Takahashi, Yu. Gravity Field Characterization around Small Bodies.

Degree: PhD, Aerospace Engineering Sciences, 2013, University of Colorado

URL: http://scholar.colorado.edu/asen_gradetds/70

► A small body rendezvous mission requires accurate gravity field characterization for safe, accurate navigation purposes. However, the current techniques of gravity field modeling around…
(more)

Subjects/Keywords: Asteroids; Comets; Gravity Field; Small Body; Aerospace Engineering; Navigation, Guidance, Control and Dynamics

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APA (6^{th} Edition):

Takahashi, Y. (2013). Gravity Field Characterization around Small Bodies. (Doctoral Dissertation). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/70

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

Takahashi, Yu. “Gravity Field Characterization around Small Bodies.” 2013. Doctoral Dissertation, University of Colorado. Accessed December 13, 2019. http://scholar.colorado.edu/asen_gradetds/70.

MLA Handbook (7^{th} Edition):

Takahashi, Yu. “Gravity Field Characterization around Small Bodies.” 2013. Web. 13 Dec 2019.

Vancouver:

Takahashi Y. Gravity Field Characterization around Small Bodies. [Internet] [Doctoral dissertation]. University of Colorado; 2013. [cited 2019 Dec 13]. Available from: http://scholar.colorado.edu/asen_gradetds/70.

Council of Science Editors:

Takahashi Y. Gravity Field Characterization around Small Bodies. [Doctoral Dissertation]. University of Colorado; 2013. Available from: http://scholar.colorado.edu/asen_gradetds/70

University of Colorado

11. Rosengren, Aaron Jay. Long-term Dynamical Behavior of Highly Perturbed Natural and Artificial Celestial Bodies.

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

URL: http://scholar.colorado.edu/asen_gradetds/79

► This thesis explores the dynamical evolution of celestial bodies, both natural and artificial, which are strongly perturbed by solar radiation pressure—a non-gravitational force that…
(more)

Subjects/Keywords: Astrodynamics; Celestial Mechanics; Classical Mechanics; Planetary Science; Space Debris; Space Situational Awareness; Astrophysics and Astronomy; Physical Processes; The Sun and the Solar System

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APA (6^{th} Edition):

Rosengren, A. J. (2014). Long-term Dynamical Behavior of Highly Perturbed Natural and Artificial Celestial Bodies. (Doctoral Dissertation). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/79

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

Rosengren, Aaron Jay. “Long-term Dynamical Behavior of Highly Perturbed Natural and Artificial Celestial Bodies.” 2014. Doctoral Dissertation, University of Colorado. Accessed December 13, 2019. http://scholar.colorado.edu/asen_gradetds/79.

MLA Handbook (7^{th} Edition):

Rosengren, Aaron Jay. “Long-term Dynamical Behavior of Highly Perturbed Natural and Artificial Celestial Bodies.” 2014. Web. 13 Dec 2019.

Vancouver:

Rosengren AJ. Long-term Dynamical Behavior of Highly Perturbed Natural and Artificial Celestial Bodies. [Internet] [Doctoral dissertation]. University of Colorado; 2014. [cited 2019 Dec 13]. Available from: http://scholar.colorado.edu/asen_gradetds/79.

Council of Science Editors:

Rosengren AJ. Long-term Dynamical Behavior of Highly Perturbed Natural and Artificial Celestial Bodies. [Doctoral Dissertation]. University of Colorado; 2014. Available from: http://scholar.colorado.edu/asen_gradetds/79

University of Colorado

12. Guerrant, Daniel Vernon. Performance Quantification of Heliogyro Solar Sails Using Structural, Attitude, and Orbital Dynamics and Control Analysis.

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

URL: http://scholar.colorado.edu/asen_gradetds/101

► Solar sails enable or enhance exploration of a variety of destinations both within and without the solar system. The heliogyro solar sail architecture divides…
(more)

Subjects/Keywords: attitude control; dynamics; heliogyro; solar sail; structural dynamics; Astrodynamics; Propulsion and Power; Space Vehicles

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APA (6^{th} Edition):

Guerrant, D. V. (2015). Performance Quantification of Heliogyro Solar Sails Using Structural, Attitude, and Orbital Dynamics and Control Analysis. (Doctoral Dissertation). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/101

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

Guerrant, Daniel Vernon. “Performance Quantification of Heliogyro Solar Sails Using Structural, Attitude, and Orbital Dynamics and Control Analysis.” 2015. Doctoral Dissertation, University of Colorado. Accessed December 13, 2019. http://scholar.colorado.edu/asen_gradetds/101.

MLA Handbook (7^{th} Edition):

Guerrant, Daniel Vernon. “Performance Quantification of Heliogyro Solar Sails Using Structural, Attitude, and Orbital Dynamics and Control Analysis.” 2015. Web. 13 Dec 2019.

Vancouver:

Guerrant DV. Performance Quantification of Heliogyro Solar Sails Using Structural, Attitude, and Orbital Dynamics and Control Analysis. [Internet] [Doctoral dissertation]. University of Colorado; 2015. [cited 2019 Dec 13]. Available from: http://scholar.colorado.edu/asen_gradetds/101.

Council of Science Editors:

Guerrant DV. Performance Quantification of Heliogyro Solar Sails Using Structural, Attitude, and Orbital Dynamics and Control Analysis. [Doctoral Dissertation]. University of Colorado; 2015. Available from: http://scholar.colorado.edu/asen_gradetds/101

University of Colorado

13. 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: http://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

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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 http://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 December 13, 2019. http://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. 13 Dec 2019.

Vancouver:

Ko HC. Representation of Unknown and Unmodeled Space Events for Satellites : Characteristics and Applications. [Internet] [Doctoral dissertation]. University of Colorado; 2015. [cited 2019 Dec 13]. Available from: http://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: http://scholar.colorado.edu/asen_gradetds/120

University of Colorado

14. Bradley, Ben K. Numerical Algorithms for Precise and Efficient Orbit Propagation and Positioning.

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

URL: http://scholar.colorado.edu/asen_gradetds/125

► Motivated by the growing space catalog and the demands for precise orbit determination with shorter latency for science and reconnaissance missions, this research improves…
(more)

Subjects/Keywords: Earth orientation parameters; International Terrestrial Reference System; Orbit propagation; Precise frame transformations; Navigation, Guidance, Control and Dynamics

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APA (6^{th} Edition):

Bradley, B. K. (2015). Numerical Algorithms for Precise and Efficient Orbit Propagation and Positioning. (Doctoral Dissertation). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/125

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

Bradley, Ben K. “Numerical Algorithms for Precise and Efficient Orbit Propagation and Positioning.” 2015. Doctoral Dissertation, University of Colorado. Accessed December 13, 2019. http://scholar.colorado.edu/asen_gradetds/125.

MLA Handbook (7^{th} Edition):

Bradley, Ben K. “Numerical Algorithms for Precise and Efficient Orbit Propagation and Positioning.” 2015. Web. 13 Dec 2019.

Vancouver:

Bradley BK. Numerical Algorithms for Precise and Efficient Orbit Propagation and Positioning. [Internet] [Doctoral dissertation]. University of Colorado; 2015. [cited 2019 Dec 13]. Available from: http://scholar.colorado.edu/asen_gradetds/125.

Council of Science Editors:

Bradley BK. Numerical Algorithms for Precise and Efficient Orbit Propagation and Positioning. [Doctoral Dissertation]. University of Colorado; 2015. Available from: http://scholar.colorado.edu/asen_gradetds/125

University of Colorado

15. Berger, Kyle Joseph. On the Role of Collisions in the Ejection of Lunar Regolith during Spacecraft Landing.

Degree: PhD, Chemical & Biochemical Engineering, 2016, University of Colorado

URL: http://scholar.colorado.edu/chbe_gradetds/94

► Gas-solid flows are ubiquitous in nature and industry and, despite being widely studied, are still not well understood. One example of such a flow…
(more)

Subjects/Keywords: Granular Materials; Multiphase Flow; Space Exploration; Chemical Engineering

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APA (6^{th} Edition):

Berger, K. J. (2016). On the Role of Collisions in the Ejection of Lunar Regolith during Spacecraft Landing. (Doctoral Dissertation). University of Colorado. Retrieved from http://scholar.colorado.edu/chbe_gradetds/94

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

Berger, Kyle Joseph. “On the Role of Collisions in the Ejection of Lunar Regolith during Spacecraft Landing.” 2016. Doctoral Dissertation, University of Colorado. Accessed December 13, 2019. http://scholar.colorado.edu/chbe_gradetds/94.

MLA Handbook (7^{th} Edition):

Berger, Kyle Joseph. “On the Role of Collisions in the Ejection of Lunar Regolith during Spacecraft Landing.” 2016. Web. 13 Dec 2019.

Vancouver:

Berger KJ. On the Role of Collisions in the Ejection of Lunar Regolith during Spacecraft Landing. [Internet] [Doctoral dissertation]. University of Colorado; 2016. [cited 2019 Dec 13]. Available from: http://scholar.colorado.edu/chbe_gradetds/94.

Council of Science Editors:

Berger KJ. On the Role of Collisions in the Ejection of Lunar Regolith during Spacecraft Landing. [Doctoral Dissertation]. University of Colorado; 2016. Available from: http://scholar.colorado.edu/chbe_gradetds/94

University of Colorado

16. Park, Inkwan. Dynamical Realism and Uncertainty Propagation.

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

URL: http://scholar.colorado.edu/asen_gradetds/130

► In recent years, Space Situational Awareness (SSA) has become increasingly important as the number of tracked Resident Space Objects (RSOs) continues their growth. One…
(more)

Subjects/Keywords: Deprit-Lie transformation; precision of dynamics; semi-analytic approach; space situational awareness; state transition tensor; uncertainty propagation; Systems Engineering and Multidisciplinary Design Optimization

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APA (6^{th} Edition):

Park, I. (2015). Dynamical Realism and Uncertainty Propagation. (Doctoral Dissertation). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/130

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

Park, Inkwan. “Dynamical Realism and Uncertainty Propagation.” 2015. Doctoral Dissertation, University of Colorado. Accessed December 13, 2019. http://scholar.colorado.edu/asen_gradetds/130.

MLA Handbook (7^{th} Edition):

Park, Inkwan. “Dynamical Realism and Uncertainty Propagation.” 2015. Web. 13 Dec 2019.

Vancouver:

Park I. Dynamical Realism and Uncertainty Propagation. [Internet] [Doctoral dissertation]. University of Colorado; 2015. [cited 2019 Dec 13]. Available from: http://scholar.colorado.edu/asen_gradetds/130.

Council of Science Editors:

Park I. Dynamical Realism and Uncertainty Propagation. [Doctoral Dissertation]. University of Colorado; 2015. Available from: http://scholar.colorado.edu/asen_gradetds/130

University of Colorado

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

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

URL: http://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

Record Details Similar Records

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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 http://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 December 13, 2019. http://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. 13 Dec 2019.

Vancouver:

Hesar SG. A Framework for Precise Orbit Determination of Small Body Orbiting Spacecraft. [Internet] [Doctoral dissertation]. University of Colorado; 2016. [cited 2019 Dec 13]. Available from: http://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: http://scholar.colorado.edu/asen_gradetds/141

University of Colorado

18. Surovik, David Allen. Autonomous Mission Design in Extreme Orbit Environments.

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

URL: http://scholar.colorado.edu/asen_gradetds/143

► An algorithm for autonomous online mission design at asteroids, comets, and small moons is developed to meet the novel challenges of their complex non-Keplerian…
(more)

Subjects/Keywords: astrodynamics; autonomy; heuristic search; mission design; motion planning; receding horizon control; Aerospace Engineering; Artificial Intelligence and Robotics; Astrodynamics; Dynamics and Dynamical Systems; Robotics

Record Details Similar Records

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

APA (6^{th} Edition):

Surovik, D. A. (2016). Autonomous Mission Design in Extreme Orbit Environments. (Doctoral Dissertation). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/143

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

Surovik, David Allen. “Autonomous Mission Design in Extreme Orbit Environments.” 2016. Doctoral Dissertation, University of Colorado. Accessed December 13, 2019. http://scholar.colorado.edu/asen_gradetds/143.

MLA Handbook (7^{th} Edition):

Surovik, David Allen. “Autonomous Mission Design in Extreme Orbit Environments.” 2016. Web. 13 Dec 2019.

Vancouver:

Surovik DA. Autonomous Mission Design in Extreme Orbit Environments. [Internet] [Doctoral dissertation]. University of Colorado; 2016. [cited 2019 Dec 13]. Available from: http://scholar.colorado.edu/asen_gradetds/143.

Council of Science Editors:

Surovik DA. Autonomous Mission Design in Extreme Orbit Environments. [Doctoral Dissertation]. University of Colorado; 2016. Available from: http://scholar.colorado.edu/asen_gradetds/143

University of Colorado

19. 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: http://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 http://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 December 13, 2019. http://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. 13 Dec 2019.

Vancouver:

Olikara ZP. Computation of Quasi-Periodic Tori and Heteroclinic Connections in Astrodynamics Using Collocation Techniques. [Internet] [Doctoral dissertation]. University of Colorado; 2016. [cited 2019 Dec 13]. Available from: http://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: http://scholar.colorado.edu/asen_gradetds/144

University of Colorado

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

Degree: PhD, Aerospace Engineering Sciences, 2017, University of Colorado

URL: https://scholar.colorado.edu/asen_gradetds/176

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

Subjects/Keywords: Astrodynamics; Cluster Flight; Dynamical Systems Theory; Quasi-periodic Invariant Tori; Spacecraft Formation Flying; Aerospace Engineering; Space Vehicles

Record Details Similar Records

❌

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

APA (6^{th} Edition):

Baresi, N. (2017). Spacecraft Formation Flight on Quasi-Periodic Invariant Tori. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/176

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

Baresi, Nicola. “Spacecraft Formation Flight on Quasi-Periodic Invariant Tori.” 2017. Doctoral Dissertation, University of Colorado. Accessed December 13, 2019. https://scholar.colorado.edu/asen_gradetds/176.

MLA Handbook (7^{th} Edition):

Baresi, Nicola. “Spacecraft Formation Flight on Quasi-Periodic Invariant Tori.” 2017. Web. 13 Dec 2019.

Vancouver:

Baresi N. Spacecraft Formation Flight on Quasi-Periodic Invariant Tori. [Internet] [Doctoral dissertation]. University of Colorado; 2017. [cited 2019 Dec 13]. Available from: https://scholar.colorado.edu/asen_gradetds/176.

Council of Science Editors:

Baresi N. Spacecraft Formation Flight on Quasi-Periodic Invariant Tori. [Doctoral Dissertation]. University of Colorado; 2017. Available from: https://scholar.colorado.edu/asen_gradetds/176

University of Colorado

21. 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

Record Details Similar Records

❌

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

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 December 13, 2019. 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. 13 Dec 2019.

Vancouver:

De Smet S. On the Design of Solar Gravity Driven Planetocentric Transfers Using Artificial Neural Networks. [Internet] [Doctoral dissertation]. University of Colorado; 2018. [cited 2019 Dec 13]. 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

22. 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

Record Details Similar Records

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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 December 13, 2019. https://scholar.colorado.edu/asen_gradetds/210.

MLA Handbook (7^{th} Edition):

Aziz, Jonathan David. “Low-Thrust Many-Revolution Trajectory Optimization.” 2018. Web. 13 Dec 2019.

Vancouver:

Aziz JD. Low-Thrust Many-Revolution Trajectory Optimization. [Internet] [Doctoral dissertation]. University of Colorado; 2018. [cited 2019 Dec 13]. 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

23. 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 December 13, 2019. 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. 13 Dec 2019.

Vancouver:

Parrish NLO. Low Thrust Trajectory Optimization in Cislunar and Translunar Space. [Internet] [Doctoral dissertation]. University of Colorado; 2018. [cited 2019 Dec 13]. 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

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

Degree: PhD, 2017, University of Colorado

URL: https://scholar.colorado.edu/asen_gradetds/219

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

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

Record Details Similar Records

❌

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

APA (6^{th} Edition):

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

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

Baresi, Nicola. “Spacecraft Formation Flight on Quasi-Periodic Invariant Tori.” 2017. Doctoral Dissertation, University of Colorado. Accessed December 13, 2019. https://scholar.colorado.edu/asen_gradetds/219.

MLA Handbook (7^{th} Edition):

Baresi, Nicola. “Spacecraft Formation Flight on Quasi-Periodic Invariant Tori.” 2017. Web. 13 Dec 2019.

Vancouver:

Baresi N. Spacecraft Formation Flight on Quasi-Periodic Invariant Tori. [Internet] [Doctoral dissertation]. University of Colorado; 2017. [cited 2019 Dec 13]. Available from: https://scholar.colorado.edu/asen_gradetds/219.

Council of Science Editors:

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