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You searched for +publisher:"University of Colorado" +contributor:("Daniel Scheeres"). Showing records 1 – 10 of 10 total matches.

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University of Colorado

1. Balducci, Marc. Orbit Uncertainty Propagation with Separated Representations.

Degree: PhD, 2018, University of Colorado

 In light of recent collisions and an increasing population of objects in Earth orbit, the space situational awareness community has significant motivation to develop novel… (more)

Subjects/Keywords: separated representations; uncertainty quantification; earth orbit; avoidance maneuver; multi-element algorithm; Aerospace Engineering; Mathematics

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APA (6th Edition):

Balducci, M. (2018). Orbit Uncertainty Propagation with Separated Representations. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/236

Chicago Manual of Style (16th Edition):

Balducci, Marc. “Orbit Uncertainty Propagation with Separated Representations.” 2018. Doctoral Dissertation, University of Colorado. Accessed February 28, 2021. https://scholar.colorado.edu/asen_gradetds/236.

MLA Handbook (7th Edition):

Balducci, Marc. “Orbit Uncertainty Propagation with Separated Representations.” 2018. Web. 28 Feb 2021.

Vancouver:

Balducci M. Orbit Uncertainty Propagation with Separated Representations. [Internet] [Doctoral dissertation]. University of Colorado; 2018. [cited 2021 Feb 28]. Available from: https://scholar.colorado.edu/asen_gradetds/236.

Council of Science Editors:

Balducci M. Orbit Uncertainty Propagation with Separated Representations. [Doctoral Dissertation]. University of Colorado; 2018. Available from: https://scholar.colorado.edu/asen_gradetds/236


University of Colorado

2. 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 https://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 February 28, 2021. https://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. 28 Feb 2021.

Vancouver:

Shupe NC. Orbit Options for an Orion-Class Spacecraft Mission to a Near-Earth Object. [Internet] [Masters thesis]. University of Colorado; 2010. [cited 2021 Feb 28]. Available from: https://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: https://scholar.colorado.edu/asen_gradetds/7


University of Colorado

3. 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 https://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 February 28, 2021. https://scholar.colorado.edu/asen_gradetds/16.

MLA Handbook (7th Edition):

Panosian, Stephen. “Stiffness Analysis of the Tethered Coulomb Structure Concept and Application.” 2011. Web. 28 Feb 2021.

Vancouver:

Panosian S. Stiffness Analysis of the Tethered Coulomb Structure Concept and Application. [Internet] [Masters thesis]. University of Colorado; 2011. [cited 2021 Feb 28]. Available from: https://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: https://scholar.colorado.edu/asen_gradetds/16


University of Colorado

4. 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 https://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 February 28, 2021. https://scholar.colorado.edu/asen_gradetds/48.

MLA Handbook (7th Edition):

Hartzell, Christine M. “The Dynamics of Near-Surface Dust on Airless Bodies.” 2012. Web. 28 Feb 2021.

Vancouver:

Hartzell CM. The Dynamics of Near-Surface Dust on Airless Bodies. [Internet] [Doctoral dissertation]. University of Colorado; 2012. [cited 2021 Feb 28]. Available from: https://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: https://scholar.colorado.edu/asen_gradetds/48


University of Colorado

5. 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 February 28, 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. 28 Feb 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 Feb 28]. 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

6. 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 (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 February 28, 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. 28 Feb 2021.

Vancouver:

Feldhacker JD. Incorporating Uncertainty into Spacecraft Mission and Trajectory Design. [Internet] [Doctoral dissertation]. University of Colorado; 2016. [cited 2021 Feb 28]. 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

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

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

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Bezrouk, Collin J. “Ballistic Capture into Lunar and Martian Distant Retrograde Orbits.” 2016. Doctoral Dissertation, University of Colorado. Accessed February 28, 2021. https://scholar.colorado.edu/asen_gradetds/147.

MLA Handbook (7th Edition):

Bezrouk, Collin J. “Ballistic Capture into Lunar and Martian Distant Retrograde Orbits.” 2016. Web. 28 Feb 2021.

Vancouver:

Bezrouk CJ. Ballistic Capture into Lunar and Martian Distant Retrograde Orbits. [Internet] [Doctoral dissertation]. University of Colorado; 2016. [cited 2021 Feb 28]. Available from: https://scholar.colorado.edu/asen_gradetds/147.

Council of Science Editors:

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


University of Colorado

8. Parsay, Khashayar. Invariant Solar Sail Formations in Elliptical Sun-Synchronous Orbits.

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

  Current and past missions that study the Earth's geomagnetic tail require multiple spacecraft to fly in formation about a highly eccentric Keplerian reference orbit… (more)

Subjects/Keywords: formation flying; magnetosphere; solar sail; sun-synchronous; Aerospace Engineering; Space Vehicles

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APA (6th Edition):

Parsay, K. (2016). Invariant Solar Sail Formations in Elliptical Sun-Synchronous Orbits. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/155

Chicago Manual of Style (16th Edition):

Parsay, Khashayar. “Invariant Solar Sail Formations in Elliptical Sun-Synchronous Orbits.” 2016. Doctoral Dissertation, University of Colorado. Accessed February 28, 2021. https://scholar.colorado.edu/asen_gradetds/155.

MLA Handbook (7th Edition):

Parsay, Khashayar. “Invariant Solar Sail Formations in Elliptical Sun-Synchronous Orbits.” 2016. Web. 28 Feb 2021.

Vancouver:

Parsay K. Invariant Solar Sail Formations in Elliptical Sun-Synchronous Orbits. [Internet] [Doctoral dissertation]. University of Colorado; 2016. [cited 2021 Feb 28]. Available from: https://scholar.colorado.edu/asen_gradetds/155.

Council of Science Editors:

Parsay K. Invariant Solar Sail Formations in Elliptical Sun-Synchronous Orbits. [Doctoral Dissertation]. University of Colorado; 2016. Available from: https://scholar.colorado.edu/asen_gradetds/155


University of Colorado

9. Geeraert, Jeroen L. Multi-Satellite Orbit Determination Using Interferometric Observables with RF Localization Applications.

Degree: PhD, 2017, University of Colorado

  Very long baseline interferometry (VLBI) specifically same-beam interferometry (SBI), and dual-satellite geolocation are two fields of research not previously connected. This is due to… (more)

Subjects/Keywords: astrodynamics; geolocation; interferometry; orbit determination; Aerospace Engineering

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APA (6th Edition):

Geeraert, J. L. (2017). Multi-Satellite Orbit Determination Using Interferometric Observables with RF Localization Applications. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/192

Chicago Manual of Style (16th Edition):

Geeraert, Jeroen L. “Multi-Satellite Orbit Determination Using Interferometric Observables with RF Localization Applications.” 2017. Doctoral Dissertation, University of Colorado. Accessed February 28, 2021. https://scholar.colorado.edu/asen_gradetds/192.

MLA Handbook (7th Edition):

Geeraert, Jeroen L. “Multi-Satellite Orbit Determination Using Interferometric Observables with RF Localization Applications.” 2017. Web. 28 Feb 2021.

Vancouver:

Geeraert JL. Multi-Satellite Orbit Determination Using Interferometric Observables with RF Localization Applications. [Internet] [Doctoral dissertation]. University of Colorado; 2017. [cited 2021 Feb 28]. Available from: https://scholar.colorado.edu/asen_gradetds/192.

Council of Science Editors:

Geeraert JL. Multi-Satellite Orbit Determination Using Interferometric Observables with RF Localization Applications. [Doctoral Dissertation]. University of Colorado; 2017. Available from: https://scholar.colorado.edu/asen_gradetds/192


University of Colorado

10. Komendera, Erik. Precise Assembly of Truss Structures by Distributed Robots.

Degree: PhD, Computer Science, 2014, University of Colorado

  Assembly robots have been in operation in industry for decades, predictably repeating the same precise motions in closed workspaces to assemble products cheaply and… (more)

Subjects/Keywords: distributed robots; optimization; robotic assembly; simultaneous localization and mapping; space telescopes; truss structures; Artificial Intelligence and Robotics; Industrial Engineering; Robotics

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APA (6th Edition):

Komendera, E. (2014). Precise Assembly of Truss Structures by Distributed Robots. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/csci_gradetds/91

Chicago Manual of Style (16th Edition):

Komendera, Erik. “Precise Assembly of Truss Structures by Distributed Robots.” 2014. Doctoral Dissertation, University of Colorado. Accessed February 28, 2021. https://scholar.colorado.edu/csci_gradetds/91.

MLA Handbook (7th Edition):

Komendera, Erik. “Precise Assembly of Truss Structures by Distributed Robots.” 2014. Web. 28 Feb 2021.

Vancouver:

Komendera E. Precise Assembly of Truss Structures by Distributed Robots. [Internet] [Doctoral dissertation]. University of Colorado; 2014. [cited 2021 Feb 28]. Available from: https://scholar.colorado.edu/csci_gradetds/91.

Council of Science Editors:

Komendera E. Precise Assembly of Truss Structures by Distributed Robots. [Doctoral Dissertation]. University of Colorado; 2014. Available from: https://scholar.colorado.edu/csci_gradetds/91

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