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You searched for +publisher:"University of Colorado" +contributor:("Hanspeter Schaub"). Showing records 1 – 30 of 49 total matches.

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University of Colorado

1. Rabotin, Christopher Bertrand. Feasibility of Reusable Continuous Thrust Spacecraft for Cargo Resupply Missions to Mars.

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

  Continuous thrust propulsion systems benefit from a much greater efficiency in vacuum than chemical rockets, at the expense of lower instantaneous thrust and high… (more)

Subjects/Keywords: interplanetary; low thrust; spacecraft; trajectory design; Aerospace Engineering

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APA (6th Edition):

Rabotin, C. B. (2017). Feasibility of Reusable Continuous Thrust Spacecraft for Cargo Resupply Missions to Mars. (Masters Thesis). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/184

Chicago Manual of Style (16th Edition):

Rabotin, Christopher Bertrand. “Feasibility of Reusable Continuous Thrust Spacecraft for Cargo Resupply Missions to Mars.” 2017. Masters Thesis, University of Colorado. Accessed December 07, 2019. https://scholar.colorado.edu/asen_gradetds/184.

MLA Handbook (7th Edition):

Rabotin, Christopher Bertrand. “Feasibility of Reusable Continuous Thrust Spacecraft for Cargo Resupply Missions to Mars.” 2017. Web. 07 Dec 2019.

Vancouver:

Rabotin CB. Feasibility of Reusable Continuous Thrust Spacecraft for Cargo Resupply Missions to Mars. [Internet] [Masters thesis]. University of Colorado; 2017. [cited 2019 Dec 07]. Available from: https://scholar.colorado.edu/asen_gradetds/184.

Council of Science Editors:

Rabotin CB. Feasibility of Reusable Continuous Thrust Spacecraft for Cargo Resupply Missions to Mars. [Masters Thesis]. University of Colorado; 2017. Available from: https://scholar.colorado.edu/asen_gradetds/184


University of Colorado

2. Alcorn, John. Fully-Coupled Dynamical Jitter Modeling of Momentum Exchange Devices.

Degree: MS, 2017, University of Colorado

 A primary source of spacecraft jitter is due to mass imbalances within momentum exchange devices (MEDs) used for fine pointing, such as reaction wheels (RWs)… (more)

Subjects/Keywords: imbalance; jitter; reaction wheel; VSCMG; Aerospace Engineering; Applied Mathematics; Mechanical Engineering

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APA (6th Edition):

Alcorn, J. (2017). Fully-Coupled Dynamical Jitter Modeling of Momentum Exchange Devices. (Masters Thesis). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/162

Chicago Manual of Style (16th Edition):

Alcorn, John. “Fully-Coupled Dynamical Jitter Modeling of Momentum Exchange Devices.” 2017. Masters Thesis, University of Colorado. Accessed December 07, 2019. http://scholar.colorado.edu/asen_gradetds/162.

MLA Handbook (7th Edition):

Alcorn, John. “Fully-Coupled Dynamical Jitter Modeling of Momentum Exchange Devices.” 2017. Web. 07 Dec 2019.

Vancouver:

Alcorn J. Fully-Coupled Dynamical Jitter Modeling of Momentum Exchange Devices. [Internet] [Masters thesis]. University of Colorado; 2017. [cited 2019 Dec 07]. Available from: http://scholar.colorado.edu/asen_gradetds/162.

Council of Science Editors:

Alcorn J. Fully-Coupled Dynamical Jitter Modeling of Momentum Exchange Devices. [Masters Thesis]. University of Colorado; 2017. Available from: http://scholar.colorado.edu/asen_gradetds/162


University of Colorado

3. Diaz Ramos, Manuel Francisco. Kinematic Steering Law for Conically-Constrained Torque-Limited Spacecraft Attitude Control.

Degree: MS, 2017, University of Colorado

 Orientation constrained attitude control is a requirement in most spacecraft missions. A novel technique for attitude control of a spacecraft subjected to an arbitrary number… (more)

Subjects/Keywords: attitude control; constrained control; Lyapunov theory; Modified Rodrigues Parameters; Aerospace Engineering

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APA (6th Edition):

Diaz Ramos, M. F. (2017). Kinematic Steering Law for Conically-Constrained Torque-Limited Spacecraft Attitude Control. (Masters Thesis). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/165

Chicago Manual of Style (16th Edition):

Diaz Ramos, Manuel Francisco. “Kinematic Steering Law for Conically-Constrained Torque-Limited Spacecraft Attitude Control.” 2017. Masters Thesis, University of Colorado. Accessed December 07, 2019. http://scholar.colorado.edu/asen_gradetds/165.

MLA Handbook (7th Edition):

Diaz Ramos, Manuel Francisco. “Kinematic Steering Law for Conically-Constrained Torque-Limited Spacecraft Attitude Control.” 2017. Web. 07 Dec 2019.

Vancouver:

Diaz Ramos MF. Kinematic Steering Law for Conically-Constrained Torque-Limited Spacecraft Attitude Control. [Internet] [Masters thesis]. University of Colorado; 2017. [cited 2019 Dec 07]. Available from: http://scholar.colorado.edu/asen_gradetds/165.

Council of Science Editors:

Diaz Ramos MF. Kinematic Steering Law for Conically-Constrained Torque-Limited Spacecraft Attitude Control. [Masters Thesis]. University of Colorado; 2017. Available from: http://scholar.colorado.edu/asen_gradetds/165


University of Colorado

4. Shupe, Nathan C. Orbit Options for an Orion-Class Spacecraft Mission to a Near-Earth Object.

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

  Based on the recommendations of the Augustine Commission, President Obama has proposed a vision for U.S. human spaceflight in the post-Shuttle era which includes… (more)

Subjects/Keywords: Human Exploration; Near Earth Object; Orbits; Orion; Aerospace Engineering; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

Shupe, N. C. (2010). Orbit Options for an Orion-Class Spacecraft Mission to a Near-Earth Object. (Masters Thesis). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/7

Chicago Manual of Style (16th Edition):

Shupe, Nathan C. “Orbit Options for an Orion-Class Spacecraft Mission to a Near-Earth Object.” 2010. Masters Thesis, University of Colorado. Accessed December 07, 2019. http://scholar.colorado.edu/asen_gradetds/7.

MLA Handbook (7th Edition):

Shupe, Nathan C. “Orbit Options for an Orion-Class Spacecraft Mission to a Near-Earth Object.” 2010. Web. 07 Dec 2019.

Vancouver:

Shupe NC. Orbit Options for an Orion-Class Spacecraft Mission to a Near-Earth Object. [Internet] [Masters thesis]. University of Colorado; 2010. [cited 2019 Dec 07]. Available from: http://scholar.colorado.edu/asen_gradetds/7.

Council of Science Editors:

Shupe NC. Orbit Options for an Orion-Class Spacecraft Mission to a Near-Earth Object. [Masters Thesis]. University of Colorado; 2010. Available from: http://scholar.colorado.edu/asen_gradetds/7


University of Colorado

5. Rizvi, Farheen. Solar Sail Attitude Dynamics and Coning Control: On Developing Control Methods for Solar Sail Coning at Orbit Rate to Attain Desired Orbital Effects.

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

  In this thesis, a control method is developed for the solar sail normal vector to trace a desired circular coning trajectory at orbit rate.… (more)

Subjects/Keywords: attitude dynamics and control; coning control; control methods; Solar sail; Aerospace Engineering; Navigation, Guidance, Control and Dynamics; Space Vehicles

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APA (6th Edition):

Rizvi, F. (2010). Solar Sail Attitude Dynamics and Coning Control: On Developing Control Methods for Solar Sail Coning at Orbit Rate to Attain Desired Orbital Effects. (Masters Thesis). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/8

Chicago Manual of Style (16th Edition):

Rizvi, Farheen. “Solar Sail Attitude Dynamics and Coning Control: On Developing Control Methods for Solar Sail Coning at Orbit Rate to Attain Desired Orbital Effects.” 2010. Masters Thesis, University of Colorado. Accessed December 07, 2019. http://scholar.colorado.edu/asen_gradetds/8.

MLA Handbook (7th Edition):

Rizvi, Farheen. “Solar Sail Attitude Dynamics and Coning Control: On Developing Control Methods for Solar Sail Coning at Orbit Rate to Attain Desired Orbital Effects.” 2010. Web. 07 Dec 2019.

Vancouver:

Rizvi F. Solar Sail Attitude Dynamics and Coning Control: On Developing Control Methods for Solar Sail Coning at Orbit Rate to Attain Desired Orbital Effects. [Internet] [Masters thesis]. University of Colorado; 2010. [cited 2019 Dec 07]. Available from: http://scholar.colorado.edu/asen_gradetds/8.

Council of Science Editors:

Rizvi F. Solar Sail Attitude Dynamics and Coning Control: On Developing Control Methods for Solar Sail Coning at Orbit Rate to Attain Desired Orbital Effects. [Masters Thesis]. University of Colorado; 2010. Available from: http://scholar.colorado.edu/asen_gradetds/8


University of Colorado

6. Inampudi, Ravi Kishore. Two-Craft Coulomb Formation Study about Circular Orbits and Libration Points.

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

  This dissertation investigates the dynamics and control of a two-craft Coulomb formation in circular orbits and at libration points; it addresses relative equilibria, stability… (more)

Subjects/Keywords: Circular Orbits and Libration Points; Dynamics and Optimal Control; Formation Flying; Optimal Reconfigurations; Relative Equilibria and Stability; Two-Craft Coulomb Tether; Aerospace Engineering

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APA (6th Edition):

Inampudi, R. K. (2010). Two-Craft Coulomb Formation Study about Circular Orbits and Libration Points. (Doctoral Dissertation). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/12

Chicago Manual of Style (16th Edition):

Inampudi, Ravi Kishore. “Two-Craft Coulomb Formation Study about Circular Orbits and Libration Points.” 2010. Doctoral Dissertation, University of Colorado. Accessed December 07, 2019. http://scholar.colorado.edu/asen_gradetds/12.

MLA Handbook (7th Edition):

Inampudi, Ravi Kishore. “Two-Craft Coulomb Formation Study about Circular Orbits and Libration Points.” 2010. Web. 07 Dec 2019.

Vancouver:

Inampudi RK. Two-Craft Coulomb Formation Study about Circular Orbits and Libration Points. [Internet] [Doctoral dissertation]. University of Colorado; 2010. [cited 2019 Dec 07]. Available from: http://scholar.colorado.edu/asen_gradetds/12.

Council of Science Editors:

Inampudi RK. Two-Craft Coulomb Formation Study about Circular Orbits and Libration Points. [Doctoral Dissertation]. University of Colorado; 2010. Available from: http://scholar.colorado.edu/asen_gradetds/12


University of Colorado

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

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

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Anderson, Paul V. “Characterizing Longitude-Dependent Orbital Debris Congestion in the Geosynchronous Orbit Regime.” 2010. Doctoral Dissertation, University of Colorado. Accessed December 07, 2019. http://scholar.colorado.edu/asen_gradetds/14.

MLA Handbook (7th Edition):

Anderson, Paul V. “Characterizing Longitude-Dependent Orbital Debris Congestion in the Geosynchronous Orbit Regime.” 2010. Web. 07 Dec 2019.

Vancouver:

Anderson PV. Characterizing Longitude-Dependent Orbital Debris Congestion in the Geosynchronous Orbit Regime. [Internet] [Doctoral dissertation]. University of Colorado; 2010. [cited 2019 Dec 07]. Available from: http://scholar.colorado.edu/asen_gradetds/14.

Council of Science Editors:

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


University of Colorado

8. Panosian, Stephen. Stiffness Analysis of the Tethered Coulomb Structure Concept and Application.

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

  This thesis investigates the Tethered Coulomb Structure (TCS) concept and its operating regime for creating large space structures and for providing satellite situational awareness.… (more)

Subjects/Keywords: Coulomb; Electrostatics; Formation; Spacecraft; Tether; Aerospace Engineering; Structures and Materials

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APA (6th Edition):

Panosian, S. (2011). Stiffness Analysis of the Tethered Coulomb Structure Concept and Application. (Masters Thesis). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/16

Chicago Manual of Style (16th Edition):

Panosian, Stephen. “Stiffness Analysis of the Tethered Coulomb Structure Concept and Application.” 2011. Masters Thesis, University of Colorado. Accessed December 07, 2019. http://scholar.colorado.edu/asen_gradetds/16.

MLA Handbook (7th Edition):

Panosian, Stephen. “Stiffness Analysis of the Tethered Coulomb Structure Concept and Application.” 2011. Web. 07 Dec 2019.

Vancouver:

Panosian S. Stiffness Analysis of the Tethered Coulomb Structure Concept and Application. [Internet] [Masters thesis]. University of Colorado; 2011. [cited 2019 Dec 07]. Available from: http://scholar.colorado.edu/asen_gradetds/16.

Council of Science Editors:

Panosian S. Stiffness Analysis of the Tethered Coulomb Structure Concept and Application. [Masters Thesis]. University of Colorado; 2011. Available from: http://scholar.colorado.edu/asen_gradetds/16


University of Colorado

9. 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 07, 2019. http://scholar.colorado.edu/asen_gradetds/20.

MLA Handbook (7th Edition):

Holzinger, Marcus J. “Optimal Control Applications in Space Situational Awareness.” 2011. Web. 07 Dec 2019.

Vancouver:

Holzinger MJ. Optimal Control Applications in Space Situational Awareness. [Internet] [Doctoral dissertation]. University of Colorado; 2011. [cited 2019 Dec 07]. 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

10. Blenden, Robin M. Regenerative Power Optimal Reaction Wheel Attitude Control.

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

  The thesis work develops an instantaneous power optimal attitude control for a spacecraft utilizing an integrated reaction wheel - flywheel system allowing for energy… (more)

Subjects/Keywords: Attitude Control; Power Optimal; Reaction Wheel; Aerospace Engineering; Space Vehicles

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APA (6th Edition):

Blenden, R. M. (2011). Regenerative Power Optimal Reaction Wheel Attitude Control. (Masters Thesis). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/21

Chicago Manual of Style (16th Edition):

Blenden, Robin M. “Regenerative Power Optimal Reaction Wheel Attitude Control.” 2011. Masters Thesis, University of Colorado. Accessed December 07, 2019. http://scholar.colorado.edu/asen_gradetds/21.

MLA Handbook (7th Edition):

Blenden, Robin M. “Regenerative Power Optimal Reaction Wheel Attitude Control.” 2011. Web. 07 Dec 2019.

Vancouver:

Blenden RM. Regenerative Power Optimal Reaction Wheel Attitude Control. [Internet] [Masters thesis]. University of Colorado; 2011. [cited 2019 Dec 07]. Available from: http://scholar.colorado.edu/asen_gradetds/21.

Council of Science Editors:

Blenden RM. Regenerative Power Optimal Reaction Wheel Attitude Control. [Masters Thesis]. University of Colorado; 2011. Available from: http://scholar.colorado.edu/asen_gradetds/21


University of Colorado

11. Dunn II, Daniel James. A Hybrid Hardware & Software Simulation Environment for Relative Orbit Motion Studies.

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

  Relative orbital motion is a topic of interest to programs developing vehicles for formation flight applications such as remote inspection or autonomous rendezvous and… (more)

Subjects/Keywords: Formation Flying; Relative Orbits; Robotics; Simulation; Virtual Hardware; Aerospace Engineering; Computer Engineering; Robotics

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APA (6th Edition):

Dunn II, D. J. (2011). A Hybrid Hardware & Software Simulation Environment for Relative Orbit Motion Studies. (Masters Thesis). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/22

Chicago Manual of Style (16th Edition):

Dunn II, Daniel James. “A Hybrid Hardware & Software Simulation Environment for Relative Orbit Motion Studies.” 2011. Masters Thesis, University of Colorado. Accessed December 07, 2019. http://scholar.colorado.edu/asen_gradetds/22.

MLA Handbook (7th Edition):

Dunn II, Daniel James. “A Hybrid Hardware & Software Simulation Environment for Relative Orbit Motion Studies.” 2011. Web. 07 Dec 2019.

Vancouver:

Dunn II DJ. A Hybrid Hardware & Software Simulation Environment for Relative Orbit Motion Studies. [Internet] [Masters thesis]. University of Colorado; 2011. [cited 2019 Dec 07]. Available from: http://scholar.colorado.edu/asen_gradetds/22.

Council of Science Editors:

Dunn II DJ. A Hybrid Hardware & Software Simulation Environment for Relative Orbit Motion Studies. [Masters Thesis]. University of Colorado; 2011. Available from: http://scholar.colorado.edu/asen_gradetds/22


University of Colorado

12. Saunders, Marc. Adaptive Formation Flying Maneuvers for Multiple Relative Orbits.

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

  In order to extend and preserve the mission of an earth orbiting satellite it is imperative that the on board maneuvers do not waste… (more)

Subjects/Keywords: formation flying; multiple vehicle management; nonlinear control; optimal feedback control; relative orbits; Aerospace Engineering

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APA (6th Edition):

Saunders, M. (2011). Adaptive Formation Flying Maneuvers for Multiple Relative Orbits. (Masters Thesis). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/23

Chicago Manual of Style (16th Edition):

Saunders, Marc. “Adaptive Formation Flying Maneuvers for Multiple Relative Orbits.” 2011. Masters Thesis, University of Colorado. Accessed December 07, 2019. http://scholar.colorado.edu/asen_gradetds/23.

MLA Handbook (7th Edition):

Saunders, Marc. “Adaptive Formation Flying Maneuvers for Multiple Relative Orbits.” 2011. Web. 07 Dec 2019.

Vancouver:

Saunders M. Adaptive Formation Flying Maneuvers for Multiple Relative Orbits. [Internet] [Masters thesis]. University of Colorado; 2011. [cited 2019 Dec 07]. Available from: http://scholar.colorado.edu/asen_gradetds/23.

Council of Science Editors:

Saunders M. Adaptive Formation Flying Maneuvers for Multiple Relative Orbits. [Masters Thesis]. University of Colorado; 2011. Available from: http://scholar.colorado.edu/asen_gradetds/23


University of Colorado

13. Krening, Samantha C. Visual Spacecraft Relative Motion Control using Higher Order Geometric Moments.

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

  This thesis studies passive visual relative control for satellites. The three main problems studied are how to keep the camera pointing at the center… (more)

Subjects/Keywords: Attitude control; Geometric moments; Monocular computer vision; Passive visual relative control; Skewness; Statistical pressure snake; Aerospace Engineering

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APA (6th Edition):

Krening, S. C. (2011). Visual Spacecraft Relative Motion Control using Higher Order Geometric Moments. (Masters Thesis). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/24

Chicago Manual of Style (16th Edition):

Krening, Samantha C. “Visual Spacecraft Relative Motion Control using Higher Order Geometric Moments.” 2011. Masters Thesis, University of Colorado. Accessed December 07, 2019. http://scholar.colorado.edu/asen_gradetds/24.

MLA Handbook (7th Edition):

Krening, Samantha C. “Visual Spacecraft Relative Motion Control using Higher Order Geometric Moments.” 2011. Web. 07 Dec 2019.

Vancouver:

Krening SC. Visual Spacecraft Relative Motion Control using Higher Order Geometric Moments. [Internet] [Masters thesis]. University of Colorado; 2011. [cited 2019 Dec 07]. Available from: http://scholar.colorado.edu/asen_gradetds/24.

Council of Science Editors:

Krening SC. Visual Spacecraft Relative Motion Control using Higher Order Geometric Moments. [Masters Thesis]. University of Colorado; 2011. Available from: http://scholar.colorado.edu/asen_gradetds/24


University of Colorado

14. Tombasco, Jill. Orbit Estimation of Geosynchronous Objects Via Ground-Based and Space-Based Optical Tracking.

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

  Angles-only orbit estimation of geosynchronous objects is a unique challenge due to the dense population of clustered geosynchronous objects, the singularities of and perturbations… (more)

Subjects/Keywords: angles-only; geosynchronous; orbit dynamics; orbit estimation; space-based optical tracking; Aerospace Engineering

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APA (6th Edition):

Tombasco, J. (2011). Orbit Estimation of Geosynchronous Objects Via Ground-Based and Space-Based Optical Tracking. (Doctoral Dissertation). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/31

Chicago Manual of Style (16th Edition):

Tombasco, Jill. “Orbit Estimation of Geosynchronous Objects Via Ground-Based and Space-Based Optical Tracking.” 2011. Doctoral Dissertation, University of Colorado. Accessed December 07, 2019. http://scholar.colorado.edu/asen_gradetds/31.

MLA Handbook (7th Edition):

Tombasco, Jill. “Orbit Estimation of Geosynchronous Objects Via Ground-Based and Space-Based Optical Tracking.” 2011. Web. 07 Dec 2019.

Vancouver:

Tombasco J. Orbit Estimation of Geosynchronous Objects Via Ground-Based and Space-Based Optical Tracking. [Internet] [Doctoral dissertation]. University of Colorado; 2011. [cited 2019 Dec 07]. Available from: http://scholar.colorado.edu/asen_gradetds/31.

Council of Science Editors:

Tombasco J. Orbit Estimation of Geosynchronous Objects Via Ground-Based and Space-Based Optical Tracking. [Doctoral Dissertation]. University of Colorado; 2011. Available from: http://scholar.colorado.edu/asen_gradetds/31


University of Colorado

15. Seubert, Carl. One-Dimensional Spacecraft Formation Flight Testbed for Terrestrial Charged Relative Motion Experiments.

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

  Spacecraft operating in a desired formation offers an abundance of attractive mission capabilities. One proposed method of controlling a close formation of spacecraft is… (more)

Subjects/Keywords: Coulomb; formation; modeling; plasma; spacecraft; testbed; Aerospace Engineering

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APA (6th Edition):

Seubert, C. (2011). One-Dimensional Spacecraft Formation Flight Testbed for Terrestrial Charged Relative Motion Experiments. (Doctoral Dissertation). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/38

Chicago Manual of Style (16th Edition):

Seubert, Carl. “One-Dimensional Spacecraft Formation Flight Testbed for Terrestrial Charged Relative Motion Experiments.” 2011. Doctoral Dissertation, University of Colorado. Accessed December 07, 2019. http://scholar.colorado.edu/asen_gradetds/38.

MLA Handbook (7th Edition):

Seubert, Carl. “One-Dimensional Spacecraft Formation Flight Testbed for Terrestrial Charged Relative Motion Experiments.” 2011. Web. 07 Dec 2019.

Vancouver:

Seubert C. One-Dimensional Spacecraft Formation Flight Testbed for Terrestrial Charged Relative Motion Experiments. [Internet] [Doctoral dissertation]. University of Colorado; 2011. [cited 2019 Dec 07]. Available from: http://scholar.colorado.edu/asen_gradetds/38.

Council of Science Editors:

Seubert C. One-Dimensional Spacecraft Formation Flight Testbed for Terrestrial Charged Relative Motion Experiments. [Doctoral Dissertation]. University of Colorado; 2011. Available from: http://scholar.colorado.edu/asen_gradetds/38


University of Colorado

16. Jones, Stephanie Leigh. Negating the Yearly Eccentricity Magnitude Variation of Super-synchronous Disposal Orbits due to Solar Radiation Pressure.

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

  Solar radiation pressure alters satellites' eccentricity by accelerating and decelerating them during each orbit. The accumulated perturbation cancels yearly for geostationary satellites, but meanwhile… (more)

Subjects/Keywords: disposal orbit; eccentricity; geostationary; orbit perturbation; satellite; solar radiation pressure; Aerospace Engineering; Engineering

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APA (6th Edition):

Jones, S. L. (2013). Negating the Yearly Eccentricity Magnitude Variation of Super-synchronous Disposal Orbits due to Solar Radiation Pressure. (Masters Thesis). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/60

Chicago Manual of Style (16th Edition):

Jones, Stephanie Leigh. “Negating the Yearly Eccentricity Magnitude Variation of Super-synchronous Disposal Orbits due to Solar Radiation Pressure.” 2013. Masters Thesis, University of Colorado. Accessed December 07, 2019. http://scholar.colorado.edu/asen_gradetds/60.

MLA Handbook (7th Edition):

Jones, Stephanie Leigh. “Negating the Yearly Eccentricity Magnitude Variation of Super-synchronous Disposal Orbits due to Solar Radiation Pressure.” 2013. Web. 07 Dec 2019.

Vancouver:

Jones SL. Negating the Yearly Eccentricity Magnitude Variation of Super-synchronous Disposal Orbits due to Solar Radiation Pressure. [Internet] [Masters thesis]. University of Colorado; 2013. [cited 2019 Dec 07]. Available from: http://scholar.colorado.edu/asen_gradetds/60.

Council of Science Editors:

Jones SL. Negating the Yearly Eccentricity Magnitude Variation of Super-synchronous Disposal Orbits due to Solar Radiation Pressure. [Masters Thesis]. University of Colorado; 2013. Available from: http://scholar.colorado.edu/asen_gradetds/60


University of Colorado

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

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

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Trowbridge, Michael Aaron. “Autonomous 3D Model Generation of Orbital Debris using Point Cloud Sensors.” 2014. Masters Thesis, University of Colorado. Accessed December 07, 2019. http://scholar.colorado.edu/asen_gradetds/86.

MLA Handbook (7th Edition):

Trowbridge, Michael Aaron. “Autonomous 3D Model Generation of Orbital Debris using Point Cloud Sensors.” 2014. Web. 07 Dec 2019.

Vancouver:

Trowbridge MA. Autonomous 3D Model Generation of Orbital Debris using Point Cloud Sensors. [Internet] [Masters thesis]. University of Colorado; 2014. [cited 2019 Dec 07]. Available from: http://scholar.colorado.edu/asen_gradetds/86.

Council of Science Editors:

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


University of Colorado

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

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

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Chabot, Joshua A. “A Spherical Magnetic Dipole Actuator for Spacecraft Attitude Control.” 2015. Masters Thesis, University of Colorado. Accessed December 07, 2019. http://scholar.colorado.edu/asen_gradetds/100.

MLA Handbook (7th Edition):

Chabot, Joshua A. “A Spherical Magnetic Dipole Actuator for Spacecraft Attitude Control.” 2015. Web. 07 Dec 2019.

Vancouver:

Chabot JA. A Spherical Magnetic Dipole Actuator for Spacecraft Attitude Control. [Internet] [Masters thesis]. University of Colorado; 2015. [cited 2019 Dec 07]. Available from: http://scholar.colorado.edu/asen_gradetds/100.

Council of Science Editors:

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


University of Colorado

19. McManus, Lauren. An Investigation into Establishing a Formation of Small Satellites in a Lunar Flower Constellation.

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

  Lunar science missions such as LADEE and GRAIL achieved unprecedented measurements of the Lunar exosphere and gravity field. These missions were performed with one… (more)

Subjects/Keywords: Aerospace Engineering

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APA (6th Edition):

McManus, L. (2015). An Investigation into Establishing a Formation of Small Satellites in a Lunar Flower Constellation. (Masters Thesis). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/104

Chicago Manual of Style (16th Edition):

McManus, Lauren. “An Investigation into Establishing a Formation of Small Satellites in a Lunar Flower Constellation.” 2015. Masters Thesis, University of Colorado. Accessed December 07, 2019. http://scholar.colorado.edu/asen_gradetds/104.

MLA Handbook (7th Edition):

McManus, Lauren. “An Investigation into Establishing a Formation of Small Satellites in a Lunar Flower Constellation.” 2015. Web. 07 Dec 2019.

Vancouver:

McManus L. An Investigation into Establishing a Formation of Small Satellites in a Lunar Flower Constellation. [Internet] [Masters thesis]. University of Colorado; 2015. [cited 2019 Dec 07]. Available from: http://scholar.colorado.edu/asen_gradetds/104.

Council of Science Editors:

McManus L. An Investigation into Establishing a Formation of Small Satellites in a Lunar Flower Constellation. [Masters Thesis]. University of Colorado; 2015. Available from: http://scholar.colorado.edu/asen_gradetds/104


University of Colorado

20. Kenneally, Patrick W. High Geometric Fidelity Solar Radiation Pressure Modeling via Graphics Processing Unit.

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

  Solar radiation pressure (SRP), the force imparted on a spacecraft due to impinging solar photons, becomes a dominant dynamic perturbation for both interplanetary and… (more)

Subjects/Keywords: computer graphics; OpenGL; parallel processing; simulation; solar radiation pressure; Aerospace Engineering; Computer Sciences

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APA (6th Edition):

Kenneally, P. W. (2016). High Geometric Fidelity Solar Radiation Pressure Modeling via Graphics Processing Unit. (Masters Thesis). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/138

Chicago Manual of Style (16th Edition):

Kenneally, Patrick W. “High Geometric Fidelity Solar Radiation Pressure Modeling via Graphics Processing Unit.” 2016. Masters Thesis, University of Colorado. Accessed December 07, 2019. http://scholar.colorado.edu/asen_gradetds/138.

MLA Handbook (7th Edition):

Kenneally, Patrick W. “High Geometric Fidelity Solar Radiation Pressure Modeling via Graphics Processing Unit.” 2016. Web. 07 Dec 2019.

Vancouver:

Kenneally PW. High Geometric Fidelity Solar Radiation Pressure Modeling via Graphics Processing Unit. [Internet] [Masters thesis]. University of Colorado; 2016. [cited 2019 Dec 07]. Available from: http://scholar.colorado.edu/asen_gradetds/138.

Council of Science Editors:

Kenneally PW. High Geometric Fidelity Solar Radiation Pressure Modeling via Graphics Processing Unit. [Masters Thesis]. University of Colorado; 2016. Available from: http://scholar.colorado.edu/asen_gradetds/138


University of Colorado

21. Ingram, Gabriel J. Development and Analysis of Volume Multi-Sphere Method Model Generation Using Electric Field Fitting.

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

 Electrostatic modeling of spacecraft has wide-reaching applications such as detumbling space debris in the Geosynchronous Earth Orbit regime before docking, servicing and tugging space debris… (more)

Subjects/Keywords: Electrostatic Modeling; Multi-Sphere Method; spacecraft; space debris; Aerospace Engineering; Space Vehicles

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APA (6th Edition):

Ingram, G. J. (2017). Development and Analysis of Volume Multi-Sphere Method Model Generation Using Electric Field Fitting. (Masters Thesis). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/175

Chicago Manual of Style (16th Edition):

Ingram, Gabriel J. “Development and Analysis of Volume Multi-Sphere Method Model Generation Using Electric Field Fitting.” 2017. Masters Thesis, University of Colorado. Accessed December 07, 2019. https://scholar.colorado.edu/asen_gradetds/175.

MLA Handbook (7th Edition):

Ingram, Gabriel J. “Development and Analysis of Volume Multi-Sphere Method Model Generation Using Electric Field Fitting.” 2017. Web. 07 Dec 2019.

Vancouver:

Ingram GJ. Development and Analysis of Volume Multi-Sphere Method Model Generation Using Electric Field Fitting. [Internet] [Masters thesis]. University of Colorado; 2017. [cited 2019 Dec 07]. Available from: https://scholar.colorado.edu/asen_gradetds/175.

Council of Science Editors:

Ingram GJ. Development and Analysis of Volume Multi-Sphere Method Model Generation Using Electric Field Fitting. [Masters Thesis]. University of Colorado; 2017. Available from: https://scholar.colorado.edu/asen_gradetds/175


University of Colorado

22. Rabotin, Christopher Bertrand. Feasibility of Reusable Continuous Thrust Spacecraft for Cargo Resupply Missions to Mars.

Degree: MS, 2017, University of Colorado

  Continuous thrust propulsion systems benefit from a much greater efficiency in vacuum than chemical rockets, at the expense of lower instantaneous thrust and high… (more)

Subjects/Keywords: interplanetary; low thrust; spacecraft; trajectory design; mars; Aerospace Engineering; Power and Energy

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APA (6th Edition):

Rabotin, C. B. (2017). Feasibility of Reusable Continuous Thrust Spacecraft for Cargo Resupply Missions to Mars. (Masters Thesis). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/222

Chicago Manual of Style (16th Edition):

Rabotin, Christopher Bertrand. “Feasibility of Reusable Continuous Thrust Spacecraft for Cargo Resupply Missions to Mars.” 2017. Masters Thesis, University of Colorado. Accessed December 07, 2019. https://scholar.colorado.edu/asen_gradetds/222.

MLA Handbook (7th Edition):

Rabotin, Christopher Bertrand. “Feasibility of Reusable Continuous Thrust Spacecraft for Cargo Resupply Missions to Mars.” 2017. Web. 07 Dec 2019.

Vancouver:

Rabotin CB. Feasibility of Reusable Continuous Thrust Spacecraft for Cargo Resupply Missions to Mars. [Internet] [Masters thesis]. University of Colorado; 2017. [cited 2019 Dec 07]. Available from: https://scholar.colorado.edu/asen_gradetds/222.

Council of Science Editors:

Rabotin CB. Feasibility of Reusable Continuous Thrust Spacecraft for Cargo Resupply Missions to Mars. [Masters Thesis]. University of Colorado; 2017. Available from: https://scholar.colorado.edu/asen_gradetds/222


University of Colorado

23. Ingram, Gabriel J. Development and Analysis of Volume Multi-Sphere Method Model Generation Using Electric Field Fitting.

Degree: MS, 2017, University of Colorado

 Electrostatic modeling of spacecraft has wide-reaching applications such as detumbling space debris in the Geosynchronous Earth Orbit regime before docking, servicing and tugging space debris… (more)

Subjects/Keywords: electrostatic modeling; multi-sphere method; analysis; spacecraft; torque; Aerospace Engineering; Analysis

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APA (6th Edition):

Ingram, G. J. (2017). Development and Analysis of Volume Multi-Sphere Method Model Generation Using Electric Field Fitting. (Masters Thesis). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/224

Chicago Manual of Style (16th Edition):

Ingram, Gabriel J. “Development and Analysis of Volume Multi-Sphere Method Model Generation Using Electric Field Fitting.” 2017. Masters Thesis, University of Colorado. Accessed December 07, 2019. https://scholar.colorado.edu/asen_gradetds/224.

MLA Handbook (7th Edition):

Ingram, Gabriel J. “Development and Analysis of Volume Multi-Sphere Method Model Generation Using Electric Field Fitting.” 2017. Web. 07 Dec 2019.

Vancouver:

Ingram GJ. Development and Analysis of Volume Multi-Sphere Method Model Generation Using Electric Field Fitting. [Internet] [Masters thesis]. University of Colorado; 2017. [cited 2019 Dec 07]. Available from: https://scholar.colorado.edu/asen_gradetds/224.

Council of Science Editors:

Ingram GJ. Development and Analysis of Volume Multi-Sphere Method Model Generation Using Electric Field Fitting. [Masters Thesis]. University of Colorado; 2017. Available from: https://scholar.colorado.edu/asen_gradetds/224


University of Colorado

24. Alcorn, John. Fully-Coupled Dynamical Jitter Modeling of Momentum Exchange Devices.

Degree: MS, 2017, University of Colorado

 A primary source of spacecraft jitter is due to mass imbalances within momentum exchange devices (MEDs) used for fine pointing, such as reaction wheels (RWs)… (more)

Subjects/Keywords: imbalance; jitter; reaction wheel; vscmg; momentum exchange devices; Aerospace Engineering; Applied Mathematics; Mechanical Engineering

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APA (6th Edition):

Alcorn, J. (2017). Fully-Coupled Dynamical Jitter Modeling of Momentum Exchange Devices. (Masters Thesis). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/232

Chicago Manual of Style (16th Edition):

Alcorn, John. “Fully-Coupled Dynamical Jitter Modeling of Momentum Exchange Devices.” 2017. Masters Thesis, University of Colorado. Accessed December 07, 2019. https://scholar.colorado.edu/asen_gradetds/232.

MLA Handbook (7th Edition):

Alcorn, John. “Fully-Coupled Dynamical Jitter Modeling of Momentum Exchange Devices.” 2017. Web. 07 Dec 2019.

Vancouver:

Alcorn J. Fully-Coupled Dynamical Jitter Modeling of Momentum Exchange Devices. [Internet] [Masters thesis]. University of Colorado; 2017. [cited 2019 Dec 07]. Available from: https://scholar.colorado.edu/asen_gradetds/232.

Council of Science Editors:

Alcorn J. Fully-Coupled Dynamical Jitter Modeling of Momentum Exchange Devices. [Masters Thesis]. University of Colorado; 2017. Available from: https://scholar.colorado.edu/asen_gradetds/232


University of Colorado

25. Diaz Ramos, Manuel Francisco. Kinematic Steering Law for Conically-Constrained Torque-Limited Spacecraft Attitude Control.

Degree: MS, 2017, University of Colorado

 Orientation constrained attitude control is a requirement in most spacecraft missions. A novel technique for attitude control of a spacecraft subjected to an arbitrary number… (more)

Subjects/Keywords: attitude control; constrained control; lyapunov theory; modified rodrigues parameters; bounded-torque control; Aerospace Engineering; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

Diaz Ramos, M. F. (2017). Kinematic Steering Law for Conically-Constrained Torque-Limited Spacecraft Attitude Control. (Masters Thesis). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/233

Chicago Manual of Style (16th Edition):

Diaz Ramos, Manuel Francisco. “Kinematic Steering Law for Conically-Constrained Torque-Limited Spacecraft Attitude Control.” 2017. Masters Thesis, University of Colorado. Accessed December 07, 2019. https://scholar.colorado.edu/asen_gradetds/233.

MLA Handbook (7th Edition):

Diaz Ramos, Manuel Francisco. “Kinematic Steering Law for Conically-Constrained Torque-Limited Spacecraft Attitude Control.” 2017. Web. 07 Dec 2019.

Vancouver:

Diaz Ramos MF. Kinematic Steering Law for Conically-Constrained Torque-Limited Spacecraft Attitude Control. [Internet] [Masters thesis]. University of Colorado; 2017. [cited 2019 Dec 07]. Available from: https://scholar.colorado.edu/asen_gradetds/233.

Council of Science Editors:

Diaz Ramos MF. Kinematic Steering Law for Conically-Constrained Torque-Limited Spacecraft Attitude Control. [Masters Thesis]. University of Colorado; 2017. Available from: https://scholar.colorado.edu/asen_gradetds/233


University of Colorado

26. 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 07, 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. 07 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 07]. 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

27. Bennett, Trevor John. On-Orbit 3-Dimensional Electrostatic Detumble for Generic Spacecraft Geometries.

Degree: PhD, 2017, University of Colorado

  In recent years, there is a growing interest in active debris removal and on-orbit servicing of Earth orbiting assets. The growing need for such… (more)

Subjects/Keywords: contactless/touchless; electrostatic actuation; formation flying; orbital debris; relative navigation; Aerospace Engineering

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APA (6th Edition):

Bennett, T. J. (2017). On-Orbit 3-Dimensional Electrostatic Detumble for Generic Spacecraft Geometries. (Doctoral Dissertation). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/163

Chicago Manual of Style (16th Edition):

Bennett, Trevor John. “On-Orbit 3-Dimensional Electrostatic Detumble for Generic Spacecraft Geometries.” 2017. Doctoral Dissertation, University of Colorado. Accessed December 07, 2019. http://scholar.colorado.edu/asen_gradetds/163.

MLA Handbook (7th Edition):

Bennett, Trevor John. “On-Orbit 3-Dimensional Electrostatic Detumble for Generic Spacecraft Geometries.” 2017. Web. 07 Dec 2019.

Vancouver:

Bennett TJ. On-Orbit 3-Dimensional Electrostatic Detumble for Generic Spacecraft Geometries. [Internet] [Doctoral dissertation]. University of Colorado; 2017. [cited 2019 Dec 07]. Available from: http://scholar.colorado.edu/asen_gradetds/163.

Council of Science Editors:

Bennett TJ. On-Orbit 3-Dimensional Electrostatic Detumble for Generic Spacecraft Geometries. [Doctoral Dissertation]. University of Colorado; 2017. Available from: http://scholar.colorado.edu/asen_gradetds/163


University of Colorado

28. Hartzell, Christine M. The Dynamics of Near-Surface Dust on Airless Bodies.

Degree: PhD, Aerospace Engineering Sciences, 2012, University of Colorado

  The behavior of dust particles under the influence of electrostatic forces has been investigated near the surface of asteroids and the Moon. Dust particle… (more)

Subjects/Keywords: asteroids; cohesion; dust; electrostatic; Moon; Aerospace Engineering; Plasma and Beam Physics

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APA (6th Edition):

Hartzell, C. M. (2012). The Dynamics of Near-Surface Dust on Airless Bodies. (Doctoral Dissertation). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/48

Chicago Manual of Style (16th Edition):

Hartzell, Christine M. “The Dynamics of Near-Surface Dust on Airless Bodies.” 2012. Doctoral Dissertation, University of Colorado. Accessed December 07, 2019. http://scholar.colorado.edu/asen_gradetds/48.

MLA Handbook (7th Edition):

Hartzell, Christine M. “The Dynamics of Near-Surface Dust on Airless Bodies.” 2012. Web. 07 Dec 2019.

Vancouver:

Hartzell CM. The Dynamics of Near-Surface Dust on Airless Bodies. [Internet] [Doctoral dissertation]. University of Colorado; 2012. [cited 2019 Dec 07]. Available from: http://scholar.colorado.edu/asen_gradetds/48.

Council of Science Editors:

Hartzell CM. The Dynamics of Near-Surface Dust on Airless Bodies. [Doctoral Dissertation]. University of Colorado; 2012. Available from: http://scholar.colorado.edu/asen_gradetds/48


University of Colorado

29. Gerhardt, David Thomas. Small Satellite Passive Magnetic Attitude Control.

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

  Passive Magnetic Attitude Control (PMAC) is capable of aligning a satellite within 5 degrees of the local magnetic field at low resource cost, making… (more)

Subjects/Keywords: Attitude; Determination; Magnetic; Measurement; Passive; Simulation; Aerospace Engineering; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

Gerhardt, D. T. (2014). Small Satellite Passive Magnetic Attitude Control. (Doctoral Dissertation). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/78

Chicago Manual of Style (16th Edition):

Gerhardt, David Thomas. “Small Satellite Passive Magnetic Attitude Control.” 2014. Doctoral Dissertation, University of Colorado. Accessed December 07, 2019. http://scholar.colorado.edu/asen_gradetds/78.

MLA Handbook (7th Edition):

Gerhardt, David Thomas. “Small Satellite Passive Magnetic Attitude Control.” 2014. Web. 07 Dec 2019.

Vancouver:

Gerhardt DT. Small Satellite Passive Magnetic Attitude Control. [Internet] [Doctoral dissertation]. University of Colorado; 2014. [cited 2019 Dec 07]. Available from: http://scholar.colorado.edu/asen_gradetds/78.

Council of Science Editors:

Gerhardt DT. Small Satellite Passive Magnetic Attitude Control. [Doctoral Dissertation]. University of Colorado; 2014. Available from: http://scholar.colorado.edu/asen_gradetds/78


University of Colorado

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

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

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Jasper, Lee E Z. “Open-Loop Thrust Profile Development for Tethered Towing of Large Space Objects.” 2014. Doctoral Dissertation, University of Colorado. Accessed December 07, 2019. http://scholar.colorado.edu/asen_gradetds/82.

MLA Handbook (7th Edition):

Jasper, Lee E Z. “Open-Loop Thrust Profile Development for Tethered Towing of Large Space Objects.” 2014. Web. 07 Dec 2019.

Vancouver:

Jasper LEZ. Open-Loop Thrust Profile Development for Tethered Towing of Large Space Objects. [Internet] [Doctoral dissertation]. University of Colorado; 2014. [cited 2019 Dec 07]. Available from: http://scholar.colorado.edu/asen_gradetds/82.

Council of Science Editors:

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

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