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You searched for +publisher:"University of Colorado" +contributor:("Jeffrey Parker"). Showing records 1 – 11 of 11 total matches.

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University of Colorado

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

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

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

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

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

APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Anderson, Paul V. “Characterizing Longitude-Dependent Orbital Debris Congestion in the Geosynchronous Orbit Regime.” 2010. Doctoral Dissertation, University of Colorado. Accessed January 26, 2021. https://scholar.colorado.edu/asen_gradetds/14.

MLA Handbook (7th Edition):

Anderson, Paul V. “Characterizing Longitude-Dependent Orbital Debris Congestion in the Geosynchronous Orbit Regime.” 2010. Web. 26 Jan 2021.

Vancouver:

Anderson PV. Characterizing Longitude-Dependent Orbital Debris Congestion in the Geosynchronous Orbit Regime. [Internet] [Doctoral dissertation]. University of Colorado; 2010. [cited 2021 Jan 26]. Available from: https://scholar.colorado.edu/asen_gradetds/14.

Council of Science Editors:

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


University of Colorado

2. 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 https://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 January 26, 2021. https://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. 26 Jan 2021.

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 2021 Jan 26]. Available from: https://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: https://scholar.colorado.edu/asen_gradetds/60


University of Colorado

3. Dowling, Jennifer Lynn. Trajectory Optimization for Crewed Missions to an Earth-Moon L2 Halo Orbit.

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

  Baseline trajectories to an Earth-Moon L2 halo orbit and round trip trajectories for crewed missions have been created in support of an advanced Orion… (more)

Subjects/Keywords: crewed mission design; Earth-Moon L2; primer vector theory; trajectory optimization; Navigation, Guidance, Control and Dynamics; Space Vehicles

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APA (6th Edition):

Dowling, J. L. (2014). Trajectory Optimization for Crewed Missions to an Earth-Moon L2 Halo Orbit. (Masters Thesis). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/85

Chicago Manual of Style (16th Edition):

Dowling, Jennifer Lynn. “Trajectory Optimization for Crewed Missions to an Earth-Moon L2 Halo Orbit.” 2014. Masters Thesis, University of Colorado. Accessed January 26, 2021. https://scholar.colorado.edu/asen_gradetds/85.

MLA Handbook (7th Edition):

Dowling, Jennifer Lynn. “Trajectory Optimization for Crewed Missions to an Earth-Moon L2 Halo Orbit.” 2014. Web. 26 Jan 2021.

Vancouver:

Dowling JL. Trajectory Optimization for Crewed Missions to an Earth-Moon L2 Halo Orbit. [Internet] [Masters thesis]. University of Colorado; 2014. [cited 2021 Jan 26]. Available from: https://scholar.colorado.edu/asen_gradetds/85.

Council of Science Editors:

Dowling JL. Trajectory Optimization for Crewed Missions to an Earth-Moon L2 Halo Orbit. [Masters Thesis]. University of Colorado; 2014. Available from: https://scholar.colorado.edu/asen_gradetds/85


University of Colorado

4. 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 https://scholar.colorado.edu/asen_gradetds/100

Chicago Manual of Style (16th Edition):

Chabot, Joshua A. “A Spherical Magnetic Dipole Actuator for Spacecraft Attitude Control.” 2015. Masters Thesis, University of Colorado. Accessed January 26, 2021. https://scholar.colorado.edu/asen_gradetds/100.

MLA Handbook (7th Edition):

Chabot, Joshua A. “A Spherical Magnetic Dipole Actuator for Spacecraft Attitude Control.” 2015. Web. 26 Jan 2021.

Vancouver:

Chabot JA. A Spherical Magnetic Dipole Actuator for Spacecraft Attitude Control. [Internet] [Masters thesis]. University of Colorado; 2015. [cited 2021 Jan 26]. Available from: https://scholar.colorado.edu/asen_gradetds/100.

Council of Science Editors:

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


University of Colorado

5. 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; Physics

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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 https://scholar.colorado.edu/asen_gradetds/226

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 January 26, 2021. https://scholar.colorado.edu/asen_gradetds/226.

MLA Handbook (7th Edition):

Bennett, Trevor John. “On-Orbit 3-Dimensional Electrostatic Detumble for Generic Spacecraft Geometries.” 2017. Web. 26 Jan 2021.

Vancouver:

Bennett TJ. On-Orbit 3-Dimensional Electrostatic Detumble for Generic Spacecraft Geometries. [Internet] [Doctoral dissertation]. University of Colorado; 2017. [cited 2021 Jan 26]. Available from: https://scholar.colorado.edu/asen_gradetds/226.

Council of Science Editors:

Bennett TJ. On-Orbit 3-Dimensional Electrostatic Detumble for Generic Spacecraft Geometries. [Doctoral Dissertation]. University of Colorado; 2017. Available from: https://scholar.colorado.edu/asen_gradetds/226


University of Colorado

6. 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 https://scholar.colorado.edu/asen_gradetds/82

Chicago Manual of Style (16th Edition):

Jasper, Lee E Z. “Open-Loop Thrust Profile Development for Tethered Towing of Large Space Objects.” 2014. Doctoral Dissertation, University of Colorado. Accessed January 26, 2021. https://scholar.colorado.edu/asen_gradetds/82.

MLA Handbook (7th Edition):

Jasper, Lee E Z. “Open-Loop Thrust Profile Development for Tethered Towing of Large Space Objects.” 2014. Web. 26 Jan 2021.

Vancouver:

Jasper LEZ. Open-Loop Thrust Profile Development for Tethered Towing of Large Space Objects. [Internet] [Doctoral dissertation]. University of Colorado; 2014. [cited 2021 Jan 26]. Available from: https://scholar.colorado.edu/asen_gradetds/82.

Council of Science Editors:

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


University of Colorado

7. McGranaghan, Ryan Michael. Determining Global Ionospheric Conductivity in the Satellite and Data Assimilation Age and Assessing its Influence on the Magnetosphere-Ionosphere-Thermosphere System.

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

  This work focuses on determining how effectively the upper atmosphere, as a medium, transmits the influence of an electric field into differential charge motion… (more)

Subjects/Keywords: data assimilation; geospace system science; ionospheric conductivity; ionospheric electrodynamics; magnetosphere-ionosphere-thermosphere coupling; space sciences; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

McGranaghan, R. M. (2016). Determining Global Ionospheric Conductivity in the Satellite and Data Assimilation Age and Assessing its Influence on the Magnetosphere-Ionosphere-Thermosphere System. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/134

Chicago Manual of Style (16th Edition):

McGranaghan, Ryan Michael. “Determining Global Ionospheric Conductivity in the Satellite and Data Assimilation Age and Assessing its Influence on the Magnetosphere-Ionosphere-Thermosphere System.” 2016. Doctoral Dissertation, University of Colorado. Accessed January 26, 2021. https://scholar.colorado.edu/asen_gradetds/134.

MLA Handbook (7th Edition):

McGranaghan, Ryan Michael. “Determining Global Ionospheric Conductivity in the Satellite and Data Assimilation Age and Assessing its Influence on the Magnetosphere-Ionosphere-Thermosphere System.” 2016. Web. 26 Jan 2021.

Vancouver:

McGranaghan RM. Determining Global Ionospheric Conductivity in the Satellite and Data Assimilation Age and Assessing its Influence on the Magnetosphere-Ionosphere-Thermosphere System. [Internet] [Doctoral dissertation]. University of Colorado; 2016. [cited 2021 Jan 26]. Available from: https://scholar.colorado.edu/asen_gradetds/134.

Council of Science Editors:

McGranaghan RM. Determining Global Ionospheric Conductivity in the Satellite and Data Assimilation Age and Assessing its Influence on the Magnetosphere-Ionosphere-Thermosphere System. [Doctoral Dissertation]. University of Colorado; 2016. Available from: https://scholar.colorado.edu/asen_gradetds/134


University of Colorado

8. Feldhacker, Juliana D. Incorporating Uncertainty into Spacecraft Mission and Trajectory Design.

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

  The complex nature of many astrodynamic systems often leads to high computational costs or degraded accuracy in the analysis and design of spacecraft missions,… (more)

Subjects/Keywords: mission design; optimization under uncertainty; robust design; trajectory optimization; uncertainty quantification; Aerospace Engineering

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

APA (6th Edition):

Feldhacker, J. D. (2016). Incorporating Uncertainty into Spacecraft Mission and Trajectory Design. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/135

Chicago Manual of Style (16th Edition):

Feldhacker, Juliana D. “Incorporating Uncertainty into Spacecraft Mission and Trajectory Design.” 2016. Doctoral Dissertation, University of Colorado. Accessed January 26, 2021. https://scholar.colorado.edu/asen_gradetds/135.

MLA Handbook (7th Edition):

Feldhacker, Juliana D. “Incorporating Uncertainty into Spacecraft Mission and Trajectory Design.” 2016. Web. 26 Jan 2021.

Vancouver:

Feldhacker JD. Incorporating Uncertainty into Spacecraft Mission and Trajectory Design. [Internet] [Doctoral dissertation]. University of Colorado; 2016. [cited 2021 Jan 26]. Available from: https://scholar.colorado.edu/asen_gradetds/135.

Council of Science Editors:

Feldhacker JD. Incorporating Uncertainty into Spacecraft Mission and Trajectory Design. [Doctoral Dissertation]. University of Colorado; 2016. Available from: https://scholar.colorado.edu/asen_gradetds/135


University of Colorado

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

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

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

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

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

APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Anderson, Paul Vincent. “Characterizing Longitude-Dependent Orbital Debris Congestion in the Geosynchronous Orbit Regime.” 2015. Doctoral Dissertation, University of Colorado. Accessed January 26, 2021. https://scholar.colorado.edu/asen_gradetds/91.

MLA Handbook (7th Edition):

Anderson, Paul Vincent. “Characterizing Longitude-Dependent Orbital Debris Congestion in the Geosynchronous Orbit Regime.” 2015. Web. 26 Jan 2021.

Vancouver:

Anderson PV. Characterizing Longitude-Dependent Orbital Debris Congestion in the Geosynchronous Orbit Regime. [Internet] [Doctoral dissertation]. University of Colorado; 2015. [cited 2021 Jan 26]. Available from: https://scholar.colorado.edu/asen_gradetds/91.

Council of Science Editors:

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


University of Colorado

10. 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 https://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 January 26, 2021. https://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. 26 Jan 2021.

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 2021 Jan 26]. Available from: https://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: https://scholar.colorado.edu/asen_gradetds/114


University of Colorado

11. Washburn, Scott Allen. A Model for the Rapid Evaluation of Active Magnetic Shielding Designs.

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

  The use of active magnetic radiation shielding designs has the potential to reduce the radiation exposure received by astronauts on deep-space missions at a… (more)

Subjects/Keywords: Active Shielding; GCR; Magnetic Shielding; Space Radiation Exposure; Space Radiation Shielding; Aerospace Engineering

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APA (6th Edition):

Washburn, S. A. (2013). A Model for the Rapid Evaluation of Active Magnetic Shielding Designs. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/72

Chicago Manual of Style (16th Edition):

Washburn, Scott Allen. “A Model for the Rapid Evaluation of Active Magnetic Shielding Designs.” 2013. Doctoral Dissertation, University of Colorado. Accessed January 26, 2021. https://scholar.colorado.edu/asen_gradetds/72.

MLA Handbook (7th Edition):

Washburn, Scott Allen. “A Model for the Rapid Evaluation of Active Magnetic Shielding Designs.” 2013. Web. 26 Jan 2021.

Vancouver:

Washburn SA. A Model for the Rapid Evaluation of Active Magnetic Shielding Designs. [Internet] [Doctoral dissertation]. University of Colorado; 2013. [cited 2021 Jan 26]. Available from: https://scholar.colorado.edu/asen_gradetds/72.

Council of Science Editors:

Washburn SA. A Model for the Rapid Evaluation of Active Magnetic Shielding Designs. [Doctoral Dissertation]. University of Colorado; 2013. Available from: https://scholar.colorado.edu/asen_gradetds/72

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