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You searched for +publisher:"University of Colorado" +contributor:("Daniel J. Scheeres"). Showing records 1 – 24 of 24 total matches.

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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

  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 (6th 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 (16th 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 (7th 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

  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 (6th 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 (16th 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 (7th 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

  Solar radiation pressure is the largest non-gravitational perturbation for most satellites in the solar system, and can therefore have a significant influence on their… (more)

Subjects/Keywords: astrodynamics; BYORP; celestial mechanics; orbital dynamics; orbit determination; solar radiation pressure; Aerospace Engineering; Astrodynamics

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APA (6th Edition):

McMahon, J. W. (2011). An Analytical Theory for the Perturbative Effect of Solar Radiation Pressure on Natural and Artificial Satellites. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/26

Chicago Manual of Style (16th Edition):

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

MLA Handbook (7th Edition):

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

  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 (6th 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 (16th 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 (7th 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

  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 (6th 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 (16th 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 (7th 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

  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 (6th 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 (16th 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 (7th 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

  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 (6th 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 (16th 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 (7th 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

  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 (6th 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 (16th 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 (7th 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

  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 (6th 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 (16th 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 (7th 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

  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 (6th 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 (16th 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 (7th 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

  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 (6th 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 (16th 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 (7th 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

  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 (6th 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 (16th 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 (7th 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

  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 (6th 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 (16th 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 (7th 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

  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 (6th 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 (16th 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 (7th 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

  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 (6th 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 (16th 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 (7th 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

  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 (6th 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 (16th 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 (7th 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

  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 (6th 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 (16th 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 (7th 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

  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

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

APA (6th 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 (16th 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 (7th 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

 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

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APA (6th 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 (16th 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 (7th 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

  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

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

APA (6th 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 (16th 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 (7th 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

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

APA (6th 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 (16th 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 (7th 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

  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 (6th 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 (16th 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 (7th 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

  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

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

APA (6th 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 (16th 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 (7th 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

  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

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

APA (6th 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 (16th 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 (7th 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

.