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You searched for subject:(Solar Sail). Showing records 1 – 29 of 29 total matches.

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Stellenbosch University

1. Jordaan, Willem Hendrik. Spinning solar sail : the deployment and control of a spinning solar sail satellite.

Degree: D.Phil, Electrical and Electronic Engineering, 2016, Stellenbosch University

 ENGLISH ABSTRACT: Solar sailing has become a viable and practical option for current satellite missions. A spinning solar sail has a number advantages above a… (more)

Subjects/Keywords: Solar sails; UCTD; Spin (Aerodynamics); Solar sail satellite

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APA (6th Edition):

Jordaan, W. H. (2016). Spinning solar sail : the deployment and control of a spinning solar sail satellite. (Doctoral Dissertation). Stellenbosch University. Retrieved from http://hdl.handle.net/10019.1/98477

Chicago Manual of Style (16th Edition):

Jordaan, Willem Hendrik. “Spinning solar sail : the deployment and control of a spinning solar sail satellite.” 2016. Doctoral Dissertation, Stellenbosch University. Accessed January 24, 2021. http://hdl.handle.net/10019.1/98477.

MLA Handbook (7th Edition):

Jordaan, Willem Hendrik. “Spinning solar sail : the deployment and control of a spinning solar sail satellite.” 2016. Web. 24 Jan 2021.

Vancouver:

Jordaan WH. Spinning solar sail : the deployment and control of a spinning solar sail satellite. [Internet] [Doctoral dissertation]. Stellenbosch University; 2016. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/10019.1/98477.

Council of Science Editors:

Jordaan WH. Spinning solar sail : the deployment and control of a spinning solar sail satellite. [Doctoral Dissertation]. Stellenbosch University; 2016. Available from: http://hdl.handle.net/10019.1/98477


Stellenbosch University

2. Hibbert, Luke Thirkell. The deployment of a spinning solar sail.

Degree: MEng, Electrical and Electronic Engineering, 2019, Stellenbosch University

 ENGLISH ABSTRACT: In recent years, interest in solar sailing has grown greatly, and significant research and resources are being contributed to its development and the… (more)

Subjects/Keywords: The Deployment of a Spinning Solar Sail; UCTD; Solar sails; Solar radiation  – Pressure

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APA (6th Edition):

Hibbert, L. T. (2019). The deployment of a spinning solar sail. (Thesis). Stellenbosch University. Retrieved from http://hdl.handle.net/10019.1/105819

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Hibbert, Luke Thirkell. “The deployment of a spinning solar sail.” 2019. Thesis, Stellenbosch University. Accessed January 24, 2021. http://hdl.handle.net/10019.1/105819.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Hibbert, Luke Thirkell. “The deployment of a spinning solar sail.” 2019. Web. 24 Jan 2021.

Vancouver:

Hibbert LT. The deployment of a spinning solar sail. [Internet] [Thesis]. Stellenbosch University; 2019. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/10019.1/105819.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Hibbert LT. The deployment of a spinning solar sail. [Thesis]. Stellenbosch University; 2019. Available from: http://hdl.handle.net/10019.1/105819

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


North Carolina State University

3. Hays, Scott. A Study of the Advantages of Using a Tether Ballast Mass as Part of the Control System in a Solar Sail Based Solar Storm Warning Mission.

Degree: MS, Aerospace Engineering, 2007, North Carolina State University

Subjects/Keywords: spacecraft; controls; solar sail; dynamics

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APA (6th Edition):

Hays, S. (2007). A Study of the Advantages of Using a Tether Ballast Mass as Part of the Control System in a Solar Sail Based Solar Storm Warning Mission. (Thesis). North Carolina State University. Retrieved from http://www.lib.ncsu.edu/resolver/1840.16/604

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Hays, Scott. “A Study of the Advantages of Using a Tether Ballast Mass as Part of the Control System in a Solar Sail Based Solar Storm Warning Mission.” 2007. Thesis, North Carolina State University. Accessed January 24, 2021. http://www.lib.ncsu.edu/resolver/1840.16/604.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Hays, Scott. “A Study of the Advantages of Using a Tether Ballast Mass as Part of the Control System in a Solar Sail Based Solar Storm Warning Mission.” 2007. Web. 24 Jan 2021.

Vancouver:

Hays S. A Study of the Advantages of Using a Tether Ballast Mass as Part of the Control System in a Solar Sail Based Solar Storm Warning Mission. [Internet] [Thesis]. North Carolina State University; 2007. [cited 2021 Jan 24]. Available from: http://www.lib.ncsu.edu/resolver/1840.16/604.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Hays S. A Study of the Advantages of Using a Tether Ballast Mass as Part of the Control System in a Solar Sail Based Solar Storm Warning Mission. [Thesis]. North Carolina State University; 2007. Available from: http://www.lib.ncsu.edu/resolver/1840.16/604

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Purdue University

4. Das, Ashwati. Solar Sail Trajectory Design In The Earth-Moon Circular Restricted Three Body Problem.

Degree: MS, Aeronautics and Astronautics, 2014, Purdue University

  The quest to explore the Moon has helped resolve scientific questions, has spurred leaps in technology development, and has revealed Earth's celestial companion to… (more)

Subjects/Keywords: Applied sciences; Occultation; Sail; Solar; Steering; Transfer; Turn; Aerospace Engineering

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APA (6th Edition):

Das, A. (2014). Solar Sail Trajectory Design In The Earth-Moon Circular Restricted Three Body Problem. (Thesis). Purdue University. Retrieved from http://docs.lib.purdue.edu/open_access_theses/316

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Das, Ashwati. “Solar Sail Trajectory Design In The Earth-Moon Circular Restricted Three Body Problem.” 2014. Thesis, Purdue University. Accessed January 24, 2021. http://docs.lib.purdue.edu/open_access_theses/316.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Das, Ashwati. “Solar Sail Trajectory Design In The Earth-Moon Circular Restricted Three Body Problem.” 2014. Web. 24 Jan 2021.

Vancouver:

Das A. Solar Sail Trajectory Design In The Earth-Moon Circular Restricted Three Body Problem. [Internet] [Thesis]. Purdue University; 2014. [cited 2021 Jan 24]. Available from: http://docs.lib.purdue.edu/open_access_theses/316.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Das A. Solar Sail Trajectory Design In The Earth-Moon Circular Restricted Three Body Problem. [Thesis]. Purdue University; 2014. Available from: http://docs.lib.purdue.edu/open_access_theses/316

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


University of Arizona

5. Bowers, Kade. Radiometric Modeling for Breakthrough Starshot: How Sail Shape and BRDF Impact the Adaptive Optics .

Degree: 2020, University of Arizona

 The Breakthrough Starshot program is an ambitious project to achieve interstellar travel by using a massive laser array to propel a nanocraft to 20% the… (more)

Subjects/Keywords: Adaptive Optics; BRDF; Breakthrough Starshot; Directed Energy; Solar Sail; Space Travel

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APA (6th Edition):

Bowers, K. (2020). Radiometric Modeling for Breakthrough Starshot: How Sail Shape and BRDF Impact the Adaptive Optics . (Masters Thesis). University of Arizona. Retrieved from http://hdl.handle.net/10150/642124

Chicago Manual of Style (16th Edition):

Bowers, Kade. “Radiometric Modeling for Breakthrough Starshot: How Sail Shape and BRDF Impact the Adaptive Optics .” 2020. Masters Thesis, University of Arizona. Accessed January 24, 2021. http://hdl.handle.net/10150/642124.

MLA Handbook (7th Edition):

Bowers, Kade. “Radiometric Modeling for Breakthrough Starshot: How Sail Shape and BRDF Impact the Adaptive Optics .” 2020. Web. 24 Jan 2021.

Vancouver:

Bowers K. Radiometric Modeling for Breakthrough Starshot: How Sail Shape and BRDF Impact the Adaptive Optics . [Internet] [Masters thesis]. University of Arizona; 2020. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/10150/642124.

Council of Science Editors:

Bowers K. Radiometric Modeling for Breakthrough Starshot: How Sail Shape and BRDF Impact the Adaptive Optics . [Masters Thesis]. University of Arizona; 2020. Available from: http://hdl.handle.net/10150/642124


University of Colorado

6. 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 January 24, 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. 24 Jan 2021.

Vancouver:

Parsay K. Invariant Solar Sail Formations in Elliptical Sun-Synchronous Orbits. [Internet] [Doctoral dissertation]. University of Colorado; 2016. [cited 2021 Jan 24]. 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


Delft University of Technology

7. Carzana, Livio (author). Laser-Enhanced Solar Sailing: Modeling and Trajectory Optimization for Interplanetary Missions.

Degree: 2017, Delft University of Technology

 When sunlight illuminates a body, a tiny pressure is exerted upon its surface due to the photons impacting on it. Such a principle forms the… (more)

Subjects/Keywords: Laser-enhanced; Solar Sail; Ideal; Trajectory; Optimization; Machine Learning; Evolutionary Neurocontrol

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APA (6th Edition):

Carzana, L. (. (2017). Laser-Enhanced Solar Sailing: Modeling and Trajectory Optimization for Interplanetary Missions. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:2c79c372-52d8-4489-93ae-1e2f7c673469

Chicago Manual of Style (16th Edition):

Carzana, Livio (author). “Laser-Enhanced Solar Sailing: Modeling and Trajectory Optimization for Interplanetary Missions.” 2017. Masters Thesis, Delft University of Technology. Accessed January 24, 2021. http://resolver.tudelft.nl/uuid:2c79c372-52d8-4489-93ae-1e2f7c673469.

MLA Handbook (7th Edition):

Carzana, Livio (author). “Laser-Enhanced Solar Sailing: Modeling and Trajectory Optimization for Interplanetary Missions.” 2017. Web. 24 Jan 2021.

Vancouver:

Carzana L(. Laser-Enhanced Solar Sailing: Modeling and Trajectory Optimization for Interplanetary Missions. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2021 Jan 24]. Available from: http://resolver.tudelft.nl/uuid:2c79c372-52d8-4489-93ae-1e2f7c673469.

Council of Science Editors:

Carzana L(. Laser-Enhanced Solar Sailing: Modeling and Trajectory Optimization for Interplanetary Missions. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:2c79c372-52d8-4489-93ae-1e2f7c673469


Cal Poly

8. Smiroldo, Jordan. Investigation into the Mitigation of the Effects of Uncertain Optical Degradation on an Interplanetary Solar Sail Mission Using a Single Model Update.

Degree: MS, Aerospace Engineering, 2013, Cal Poly

  The renewed academic interest in using solar sails as a source of spacecraft propulsion has been accompanied by a recent fervor of investigations into… (more)

Subjects/Keywords: Solar; Sail; Trajectory; Collocation; Non-ideal; Performance; Astrodynamics

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APA (6th Edition):

Smiroldo, J. (2013). Investigation into the Mitigation of the Effects of Uncertain Optical Degradation on an Interplanetary Solar Sail Mission Using a Single Model Update. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1135 ; 10.15368/theses.2013.215

Chicago Manual of Style (16th Edition):

Smiroldo, Jordan. “Investigation into the Mitigation of the Effects of Uncertain Optical Degradation on an Interplanetary Solar Sail Mission Using a Single Model Update.” 2013. Masters Thesis, Cal Poly. Accessed January 24, 2021. https://digitalcommons.calpoly.edu/theses/1135 ; 10.15368/theses.2013.215.

MLA Handbook (7th Edition):

Smiroldo, Jordan. “Investigation into the Mitigation of the Effects of Uncertain Optical Degradation on an Interplanetary Solar Sail Mission Using a Single Model Update.” 2013. Web. 24 Jan 2021.

Vancouver:

Smiroldo J. Investigation into the Mitigation of the Effects of Uncertain Optical Degradation on an Interplanetary Solar Sail Mission Using a Single Model Update. [Internet] [Masters thesis]. Cal Poly; 2013. [cited 2021 Jan 24]. Available from: https://digitalcommons.calpoly.edu/theses/1135 ; 10.15368/theses.2013.215.

Council of Science Editors:

Smiroldo J. Investigation into the Mitigation of the Effects of Uncertain Optical Degradation on an Interplanetary Solar Sail Mission Using a Single Model Update. [Masters Thesis]. Cal Poly; 2013. Available from: https://digitalcommons.calpoly.edu/theses/1135 ; 10.15368/theses.2013.215

9. Gonzales, Jorell Salazar. Finite element analysis of a solar sail affected by celestial bodies.

Degree: MS, Mechanical Engineering, 2013, California State University – Sacramento

Solar sails are spacecrafts that use light propulsion to push their large sails to accelerate forward. Just like how sailboats use the wind to move… (more)

Subjects/Keywords: Membrane; Deformation; Solar sail

…7 3. SOLAR SAIL DEFORMATION… …13 3.1. Solar Sail Construction… …13 4. Table 3.2: Applied Forces on Solar Sail… …3.3: 10 m Solar Sail Viewed in the x-y Plane. …..…....................….15 10. Figure… …Figure 3.5: Solar Sail with Applied Solar Pressure… 

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APA (6th Edition):

Gonzales, J. S. (2013). Finite element analysis of a solar sail affected by celestial bodies. (Masters Thesis). California State University – Sacramento. Retrieved from http://hdl.handle.net/10211.9/2095

Chicago Manual of Style (16th Edition):

Gonzales, Jorell Salazar. “Finite element analysis of a solar sail affected by celestial bodies.” 2013. Masters Thesis, California State University – Sacramento. Accessed January 24, 2021. http://hdl.handle.net/10211.9/2095.

MLA Handbook (7th Edition):

Gonzales, Jorell Salazar. “Finite element analysis of a solar sail affected by celestial bodies.” 2013. Web. 24 Jan 2021.

Vancouver:

Gonzales JS. Finite element analysis of a solar sail affected by celestial bodies. [Internet] [Masters thesis]. California State University – Sacramento; 2013. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/10211.9/2095.

Council of Science Editors:

Gonzales JS. Finite element analysis of a solar sail affected by celestial bodies. [Masters Thesis]. California State University – Sacramento; 2013. Available from: http://hdl.handle.net/10211.9/2095


Delft University of Technology

10. van den Oever, Tom (author). Solar-sail transfers to Earth-Moon L2-displaced vertical Lyapunov orbits.

Degree: 2018, Delft University of Technology

 This thesis presents the design of solar-sail transfer trajectories to a constellation of two spacecraft in displaced vertical Lyapunov orbits at the L2 point of… (more)

Subjects/Keywords: Collocation; Trajectory; Discretization; Earth-Moon; Astrodynamics; Solar sail; Solar-sail; Solar sailing; Mesh control; Error estimation; Soyuz; Transfer trajectory; vertical Lyapunov; orbit; Gauss-Lobatto; Gauss-Newton

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APA (6th Edition):

van den Oever, T. (. (2018). Solar-sail transfers to Earth-Moon L2-displaced vertical Lyapunov orbits. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:066162cd-c531-4400-8e0f-3b3d6dedb5b9

Chicago Manual of Style (16th Edition):

van den Oever, Tom (author). “Solar-sail transfers to Earth-Moon L2-displaced vertical Lyapunov orbits.” 2018. Masters Thesis, Delft University of Technology. Accessed January 24, 2021. http://resolver.tudelft.nl/uuid:066162cd-c531-4400-8e0f-3b3d6dedb5b9.

MLA Handbook (7th Edition):

van den Oever, Tom (author). “Solar-sail transfers to Earth-Moon L2-displaced vertical Lyapunov orbits.” 2018. Web. 24 Jan 2021.

Vancouver:

van den Oever T(. Solar-sail transfers to Earth-Moon L2-displaced vertical Lyapunov orbits. [Internet] [Masters thesis]. Delft University of Technology; 2018. [cited 2021 Jan 24]. Available from: http://resolver.tudelft.nl/uuid:066162cd-c531-4400-8e0f-3b3d6dedb5b9.

Council of Science Editors:

van den Oever T(. Solar-sail transfers to Earth-Moon L2-displaced vertical Lyapunov orbits. [Masters Thesis]. Delft University of Technology; 2018. Available from: http://resolver.tudelft.nl/uuid:066162cd-c531-4400-8e0f-3b3d6dedb5b9


Rochester Institute of Technology

11. Schuster, Daniel George, Jr. Dynamic Response of Dielectric Lenses Influenced By Radiation Pressure.

Degree: MS, Mechanical Engineering, 2014, Rochester Institute of Technology

  Through analytical modeling and numerical simulations the dynamic response and stability of dielectric lenses that are influenced by radiation pressure forces and torques is… (more)

Subjects/Keywords: Dielectric lenses; Gyroscopic motion; Mathieu equation; Radiation pressure; Solar sail; Stability and control

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APA (6th Edition):

Schuster, Daniel George, J. (2014). Dynamic Response of Dielectric Lenses Influenced By Radiation Pressure. (Masters Thesis). Rochester Institute of Technology. Retrieved from https://scholarworks.rit.edu/theses/8318

Chicago Manual of Style (16th Edition):

Schuster, Daniel George, Jr. “Dynamic Response of Dielectric Lenses Influenced By Radiation Pressure.” 2014. Masters Thesis, Rochester Institute of Technology. Accessed January 24, 2021. https://scholarworks.rit.edu/theses/8318.

MLA Handbook (7th Edition):

Schuster, Daniel George, Jr. “Dynamic Response of Dielectric Lenses Influenced By Radiation Pressure.” 2014. Web. 24 Jan 2021.

Vancouver:

Schuster, Daniel George J. Dynamic Response of Dielectric Lenses Influenced By Radiation Pressure. [Internet] [Masters thesis]. Rochester Institute of Technology; 2014. [cited 2021 Jan 24]. Available from: https://scholarworks.rit.edu/theses/8318.

Council of Science Editors:

Schuster, Daniel George J. Dynamic Response of Dielectric Lenses Influenced By Radiation Pressure. [Masters Thesis]. Rochester Institute of Technology; 2014. Available from: https://scholarworks.rit.edu/theses/8318


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 https://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 January 24, 2021. https://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. 24 Jan 2021.

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 2021 Jan 24]. Available from: https://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: https://scholar.colorado.edu/asen_gradetds/101


University of Toronto

13. Choi, Mirue. Flexible Dynamics and Attitude Control of a Square Solar Sail.

Degree: PhD, 2015, University of Toronto

 This thesis presents a comprehensive analysis of attitude and structural dynamics of a square solar sail. In particular, this research examines the use of corner-attached… (more)

Subjects/Keywords: Attitude Control; Control Allocation; Finite Element Method; Flexible Dynamics; Solar Sail; Wrinkling; 0538

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APA (6th Edition):

Choi, M. (2015). Flexible Dynamics and Attitude Control of a Square Solar Sail. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/69253

Chicago Manual of Style (16th Edition):

Choi, Mirue. “Flexible Dynamics and Attitude Control of a Square Solar Sail.” 2015. Doctoral Dissertation, University of Toronto. Accessed January 24, 2021. http://hdl.handle.net/1807/69253.

MLA Handbook (7th Edition):

Choi, Mirue. “Flexible Dynamics and Attitude Control of a Square Solar Sail.” 2015. Web. 24 Jan 2021.

Vancouver:

Choi M. Flexible Dynamics and Attitude Control of a Square Solar Sail. [Internet] [Doctoral dissertation]. University of Toronto; 2015. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/1807/69253.

Council of Science Editors:

Choi M. Flexible Dynamics and Attitude Control of a Square Solar Sail. [Doctoral Dissertation]. University of Toronto; 2015. Available from: http://hdl.handle.net/1807/69253

14. -3389-7219. Uncertainty management in solar sail attitude control.

Degree: PhD, Aerospace engineering, 2016, University of Texas – Austin

Solar sails are emerging as a viable alternative to conventional forms of propulsion. Still at their infancy and relatively untested, many sources of uncertainty remain… (more)

Subjects/Keywords: Solar sail; Attitude control; Uncertainty

…5 Chapter 2 Propellantless Attitude Control of a Nonplanar Solar Sail… …sailing which shifted towards design of a solar sail that could rendezvous with the Halley comet… …orbits, the ratio of solar sail area to overall spacecraft mass must remain high and in fact… …effort to increase solar sail size and performance as highlighted by NASA’s technology roadmap… …decreased due to miniaturization technologies. Current solar sail designs have been modestly sized… 

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APA (6th Edition):

-3389-7219. (2016). Uncertainty management in solar sail attitude control. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/46779

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Chicago Manual of Style (16th Edition):

-3389-7219. “Uncertainty management in solar sail attitude control.” 2016. Doctoral Dissertation, University of Texas – Austin. Accessed January 24, 2021. http://hdl.handle.net/2152/46779.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

MLA Handbook (7th Edition):

-3389-7219. “Uncertainty management in solar sail attitude control.” 2016. Web. 24 Jan 2021.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Vancouver:

-3389-7219. Uncertainty management in solar sail attitude control. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2016. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/2152/46779.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Council of Science Editors:

-3389-7219. Uncertainty management in solar sail attitude control. [Doctoral Dissertation]. University of Texas – Austin; 2016. Available from: http://hdl.handle.net/2152/46779

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete


Purdue University

15. Sood, Rohan. Significance of Specific Force Models in Two Applications: Solar Sails to Sun-Earth L4/L5 and GRAIL Data Analysis Suggesting Lava Tubes and Buried Craters on the Moon.

Degree: PhD, Aeronautics and Astronautics, 2016, Purdue University

 In the trajectory design process, gravitational interaction between the bodies of interest plays a key role in developing the over-arching force model. However, non-gravitational forces,… (more)

Subjects/Keywords: buried crater; lava tube; low enery transfer trajectories; moon; solar sail; trajectory design

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APA (6th Edition):

Sood, R. (2016). Significance of Specific Force Models in Two Applications: Solar Sails to Sun-Earth L4/L5 and GRAIL Data Analysis Suggesting Lava Tubes and Buried Craters on the Moon. (Doctoral Dissertation). Purdue University. Retrieved from https://docs.lib.purdue.edu/open_access_dissertations/1374

Chicago Manual of Style (16th Edition):

Sood, Rohan. “Significance of Specific Force Models in Two Applications: Solar Sails to Sun-Earth L4/L5 and GRAIL Data Analysis Suggesting Lava Tubes and Buried Craters on the Moon.” 2016. Doctoral Dissertation, Purdue University. Accessed January 24, 2021. https://docs.lib.purdue.edu/open_access_dissertations/1374.

MLA Handbook (7th Edition):

Sood, Rohan. “Significance of Specific Force Models in Two Applications: Solar Sails to Sun-Earth L4/L5 and GRAIL Data Analysis Suggesting Lava Tubes and Buried Craters on the Moon.” 2016. Web. 24 Jan 2021.

Vancouver:

Sood R. Significance of Specific Force Models in Two Applications: Solar Sails to Sun-Earth L4/L5 and GRAIL Data Analysis Suggesting Lava Tubes and Buried Craters on the Moon. [Internet] [Doctoral dissertation]. Purdue University; 2016. [cited 2021 Jan 24]. Available from: https://docs.lib.purdue.edu/open_access_dissertations/1374.

Council of Science Editors:

Sood R. Significance of Specific Force Models in Two Applications: Solar Sails to Sun-Earth L4/L5 and GRAIL Data Analysis Suggesting Lava Tubes and Buried Craters on the Moon. [Doctoral Dissertation]. Purdue University; 2016. Available from: https://docs.lib.purdue.edu/open_access_dissertations/1374

16. Maria Cecilia Pereira de Faria. Dinâmica orbital e controle de orientação de um veículo espacial com uma vela solar composta.

Degree: 2009, Instituto Nacional de Pesquisas Espaciais

Neste trabalho foi realizado um estudo das propriedades dinâmicas de um sistema propulsor que utiliza radiação solar. Foram desenvolvidos modelos de força e torque para… (more)

Subjects/Keywords: vela solar; dinâmica orbital; atitude; controle; baixo empuxo; solar sail; orbital dynamics; attitude; control; low thrust

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APA (6th Edition):

Faria, M. C. P. d. (2009). Dinâmica orbital e controle de orientação de um veículo espacial com uma vela solar composta. (Thesis). Instituto Nacional de Pesquisas Espaciais. Retrieved from http://urlib.net/sid.inpe.br/[email protected]/2009/06.17.20.21

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Faria, Maria Cecilia Pereira de. “Dinâmica orbital e controle de orientação de um veículo espacial com uma vela solar composta.” 2009. Thesis, Instituto Nacional de Pesquisas Espaciais. Accessed January 24, 2021. http://urlib.net/sid.inpe.br/[email protected]/2009/06.17.20.21.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Faria, Maria Cecilia Pereira de. “Dinâmica orbital e controle de orientação de um veículo espacial com uma vela solar composta.” 2009. Web. 24 Jan 2021.

Vancouver:

Faria MCPd. Dinâmica orbital e controle de orientação de um veículo espacial com uma vela solar composta. [Internet] [Thesis]. Instituto Nacional de Pesquisas Espaciais; 2009. [cited 2021 Jan 24]. Available from: http://urlib.net/sid.inpe.br/[email protected]/2009/06.17.20.21.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Faria MCPd. Dinâmica orbital e controle de orientação de um veículo espacial com uma vela solar composta. [Thesis]. Instituto Nacional de Pesquisas Espaciais; 2009. Available from: http://urlib.net/sid.inpe.br/[email protected]/2009/06.17.20.21

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Penn State University

17. Davis, Elizabeth. SOLAR SAIL TRAJECTORY OPTIMIZATION USING COLLOCATION AND NSGA II.

Degree: 2008, Penn State University

Solar sail spacecraft rely solely on solar radiation pressure for propulsion. Since the acceleration received by radiation pressure increases as the spacecraft nears the Sun,… (more)

Subjects/Keywords: solar sail; collocation; evolutionary algorithm; trajectory optimization; NAGA II

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APA (6th Edition):

Davis, E. (2008). SOLAR SAIL TRAJECTORY OPTIMIZATION USING COLLOCATION AND NSGA II. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/8407

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Davis, Elizabeth. “SOLAR SAIL TRAJECTORY OPTIMIZATION USING COLLOCATION AND NSGA II.” 2008. Thesis, Penn State University. Accessed January 24, 2021. https://submit-etda.libraries.psu.edu/catalog/8407.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Davis, Elizabeth. “SOLAR SAIL TRAJECTORY OPTIMIZATION USING COLLOCATION AND NSGA II.” 2008. Web. 24 Jan 2021.

Vancouver:

Davis E. SOLAR SAIL TRAJECTORY OPTIMIZATION USING COLLOCATION AND NSGA II. [Internet] [Thesis]. Penn State University; 2008. [cited 2021 Jan 24]. Available from: https://submit-etda.libraries.psu.edu/catalog/8407.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Davis E. SOLAR SAIL TRAJECTORY OPTIMIZATION USING COLLOCATION AND NSGA II. [Thesis]. Penn State University; 2008. Available from: https://submit-etda.libraries.psu.edu/catalog/8407

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


University of Colorado

18. 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 https://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 January 24, 2021. https://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. 24 Jan 2021.

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 2021 Jan 24]. Available from: https://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: https://scholar.colorado.edu/asen_gradetds/8


Delft University of Technology

19. Duran Ventas, Javier (author). Solar Sail Periodic Orbits using Taylor Series Integration: Computation and applications of solar sail periodic orbit families in the Earth-Moon and binary asteroid systems.

Degree: 2017, Delft University of Technology

Solar sailing is an innovative space propulsion system based solely on the exchange of momentum between a reflective surface and the photons radiated as light… (more)

Subjects/Keywords: Solar Sail; Orbit; Taylor Series Integration; TSI; Periodic Orbits; Earth-Moon; Binary asteroids; Differential correction; Multiple shooting

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APA (6th Edition):

Duran Ventas, J. (. (2017). Solar Sail Periodic Orbits using Taylor Series Integration: Computation and applications of solar sail periodic orbit families in the Earth-Moon and binary asteroid systems. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:ada9b18c-c006-481a-bc31-b8551c2afd99

Chicago Manual of Style (16th Edition):

Duran Ventas, Javier (author). “Solar Sail Periodic Orbits using Taylor Series Integration: Computation and applications of solar sail periodic orbit families in the Earth-Moon and binary asteroid systems.” 2017. Masters Thesis, Delft University of Technology. Accessed January 24, 2021. http://resolver.tudelft.nl/uuid:ada9b18c-c006-481a-bc31-b8551c2afd99.

MLA Handbook (7th Edition):

Duran Ventas, Javier (author). “Solar Sail Periodic Orbits using Taylor Series Integration: Computation and applications of solar sail periodic orbit families in the Earth-Moon and binary asteroid systems.” 2017. Web. 24 Jan 2021.

Vancouver:

Duran Ventas J(. Solar Sail Periodic Orbits using Taylor Series Integration: Computation and applications of solar sail periodic orbit families in the Earth-Moon and binary asteroid systems. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2021 Jan 24]. Available from: http://resolver.tudelft.nl/uuid:ada9b18c-c006-481a-bc31-b8551c2afd99.

Council of Science Editors:

Duran Ventas J(. Solar Sail Periodic Orbits using Taylor Series Integration: Computation and applications of solar sail periodic orbit families in the Earth-Moon and binary asteroid systems. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:ada9b18c-c006-481a-bc31-b8551c2afd99


University of Maryland

20. Ma, Dakang. Measurement of radiation pressure and tailored momentum transfer through switchable photonic devices.

Degree: Electrical Engineering, 2016, University of Maryland

 Light carries momentum, which can be transferred to an object upon reflection or absorption. The resulting force per unit area from light, so called radiation… (more)

Subjects/Keywords: Optics; Physics; Electromagnetics; microcantilever; photon momentum; polymer dispersed liquid crystal; radiation pressure; solar sail; switchable material

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APA (6th Edition):

Ma, D. (2016). Measurement of radiation pressure and tailored momentum transfer through switchable photonic devices. (Thesis). University of Maryland. Retrieved from http://hdl.handle.net/1903/19291

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Ma, Dakang. “Measurement of radiation pressure and tailored momentum transfer through switchable photonic devices.” 2016. Thesis, University of Maryland. Accessed January 24, 2021. http://hdl.handle.net/1903/19291.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Ma, Dakang. “Measurement of radiation pressure and tailored momentum transfer through switchable photonic devices.” 2016. Web. 24 Jan 2021.

Vancouver:

Ma D. Measurement of radiation pressure and tailored momentum transfer through switchable photonic devices. [Internet] [Thesis]. University of Maryland; 2016. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/1903/19291.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Ma D. Measurement of radiation pressure and tailored momentum transfer through switchable photonic devices. [Thesis]. University of Maryland; 2016. Available from: http://hdl.handle.net/1903/19291

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


The Ohio State University

21. Gero, Ryan Micah. Low-Impact and Damped State Feedback Control of a Solar Sail on an Optimal Non-Keplerian Planet-Centered Orbit.

Degree: MS, Aeronautical and Astronautical Engineering, 2009, The Ohio State University

  Consider the most fundamental difference between a solar sail and conventional spacecraft: propellant. In order to effect propulsion, solar sails receive a constant supply… (more)

Subjects/Keywords: Astrophysics; Engineering; solar sail; optimal non-Keplerian planet-centered orbit; solar sail control; damped state feedback control; astrophysics

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APA (6th Edition):

Gero, R. M. (2009). Low-Impact and Damped State Feedback Control of a Solar Sail on an Optimal Non-Keplerian Planet-Centered Orbit. (Masters Thesis). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1243426802

Chicago Manual of Style (16th Edition):

Gero, Ryan Micah. “Low-Impact and Damped State Feedback Control of a Solar Sail on an Optimal Non-Keplerian Planet-Centered Orbit.” 2009. Masters Thesis, The Ohio State University. Accessed January 24, 2021. http://rave.ohiolink.edu/etdc/view?acc_num=osu1243426802.

MLA Handbook (7th Edition):

Gero, Ryan Micah. “Low-Impact and Damped State Feedback Control of a Solar Sail on an Optimal Non-Keplerian Planet-Centered Orbit.” 2009. Web. 24 Jan 2021.

Vancouver:

Gero RM. Low-Impact and Damped State Feedback Control of a Solar Sail on an Optimal Non-Keplerian Planet-Centered Orbit. [Internet] [Masters thesis]. The Ohio State University; 2009. [cited 2021 Jan 24]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1243426802.

Council of Science Editors:

Gero RM. Low-Impact and Damped State Feedback Control of a Solar Sail on an Optimal Non-Keplerian Planet-Centered Orbit. [Masters Thesis]. The Ohio State University; 2009. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1243426802


York University

22. Li, Gangqiang. Multibody Dynamics and Control of Tethered Spacecraft Systems.

Degree: PhD, Earth & Space Science, 2019, York University

 This doctoral research conducts high-fidelity multiphysics modeling for tethered spacecraft systems, such as electrodynamic tether systems, electric solar wind sail systems, and tether transportation systems… (more)

Subjects/Keywords: Computer engineering; Finite element method; Tethered spacecraft systems; Control; Dynamics; Electric solar wind sail; Tether transportation system; Partial space elevator; Space elevator; Electrodynamic tether systems

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APA (6th Edition):

Li, G. (2019). Multibody Dynamics and Control of Tethered Spacecraft Systems. (Doctoral Dissertation). York University. Retrieved from https://yorkspace.library.yorku.ca/xmlui/handle/10315/36739

Chicago Manual of Style (16th Edition):

Li, Gangqiang. “Multibody Dynamics and Control of Tethered Spacecraft Systems.” 2019. Doctoral Dissertation, York University. Accessed January 24, 2021. https://yorkspace.library.yorku.ca/xmlui/handle/10315/36739.

MLA Handbook (7th Edition):

Li, Gangqiang. “Multibody Dynamics and Control of Tethered Spacecraft Systems.” 2019. Web. 24 Jan 2021.

Vancouver:

Li G. Multibody Dynamics and Control of Tethered Spacecraft Systems. [Internet] [Doctoral dissertation]. York University; 2019. [cited 2021 Jan 24]. Available from: https://yorkspace.library.yorku.ca/xmlui/handle/10315/36739.

Council of Science Editors:

Li G. Multibody Dynamics and Control of Tethered Spacecraft Systems. [Doctoral Dissertation]. York University; 2019. Available from: https://yorkspace.library.yorku.ca/xmlui/handle/10315/36739

23. Hoshi, Kento. Study on Active Spacecraft Charging Model and its Application to Space Propulsion System .

Degree: 2018, Kyoto University

Subjects/Keywords: Spacecraft Charging; Space Propulsion; Plasma Simulation; Particle-in-cell; Electric Solar Wind Sail

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APA (6th Edition):

Hoshi, K. (2018). Study on Active Spacecraft Charging Model and its Application to Space Propulsion System . (Thesis). Kyoto University. Retrieved from http://hdl.handle.net/2433/232002

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Hoshi, Kento. “Study on Active Spacecraft Charging Model and its Application to Space Propulsion System .” 2018. Thesis, Kyoto University. Accessed January 24, 2021. http://hdl.handle.net/2433/232002.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Hoshi, Kento. “Study on Active Spacecraft Charging Model and its Application to Space Propulsion System .” 2018. Web. 24 Jan 2021.

Vancouver:

Hoshi K. Study on Active Spacecraft Charging Model and its Application to Space Propulsion System . [Internet] [Thesis]. Kyoto University; 2018. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/2433/232002.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Hoshi K. Study on Active Spacecraft Charging Model and its Application to Space Propulsion System . [Thesis]. Kyoto University; 2018. Available from: http://hdl.handle.net/2433/232002

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


University of Manchester

24. Wu, Rui. Self-Regulated Centrifugal Deployment of Passive Space Structures.

Degree: 2018, University of Manchester

 Large lightweight compliant structures can be spin deployed, utilising centrifugal forces to achieve a compression-free stress distribution. The present research starts from the idea that… (more)

Subjects/Keywords: deployable space structure; morphing; self regulation; intelligent system; smart material; self folding; aerodynamic decelerator; heat shield; solar sail; gossamer structure; downrange manoeuvre

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APA (6th Edition):

Wu, R. (2018). Self-Regulated Centrifugal Deployment of Passive Space Structures. (Doctoral Dissertation). University of Manchester. Retrieved from http://www.manchester.ac.uk/escholar/uk-ac-man-scw:316946

Chicago Manual of Style (16th Edition):

Wu, Rui. “Self-Regulated Centrifugal Deployment of Passive Space Structures.” 2018. Doctoral Dissertation, University of Manchester. Accessed January 24, 2021. http://www.manchester.ac.uk/escholar/uk-ac-man-scw:316946.

MLA Handbook (7th Edition):

Wu, Rui. “Self-Regulated Centrifugal Deployment of Passive Space Structures.” 2018. Web. 24 Jan 2021.

Vancouver:

Wu R. Self-Regulated Centrifugal Deployment of Passive Space Structures. [Internet] [Doctoral dissertation]. University of Manchester; 2018. [cited 2021 Jan 24]. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:316946.

Council of Science Editors:

Wu R. Self-Regulated Centrifugal Deployment of Passive Space Structures. [Doctoral Dissertation]. University of Manchester; 2018. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:316946

25. Yamaguchi, Kouhei. On Asteroid Deflection Techniques Exploiting Space Plasma Environment : 宇宙プラズマ環境を利用した小惑星の軌道変更手法に関する研究.

Degree: 博士(工学), 2017, Kyoto University / 京都大学

新制・課程博士

甲第20375号

工博第4312号

Subjects/Keywords: Asteroid deflection missions; Electric solar wind sail; Coulomb force attractor; Spacecraft charging; Kinetic impactor

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APA (6th Edition):

Yamaguchi, K. (2017). On Asteroid Deflection Techniques Exploiting Space Plasma Environment : 宇宙プラズマ環境を利用した小惑星の軌道変更手法に関する研究. (Thesis). Kyoto University / 京都大学. Retrieved from http://hdl.handle.net/2433/225600 ; http://dx.doi.org/10.14989/doctor.k20375

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Yamaguchi, Kouhei. “On Asteroid Deflection Techniques Exploiting Space Plasma Environment : 宇宙プラズマ環境を利用した小惑星の軌道変更手法に関する研究.” 2017. Thesis, Kyoto University / 京都大学. Accessed January 24, 2021. http://hdl.handle.net/2433/225600 ; http://dx.doi.org/10.14989/doctor.k20375.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Yamaguchi, Kouhei. “On Asteroid Deflection Techniques Exploiting Space Plasma Environment : 宇宙プラズマ環境を利用した小惑星の軌道変更手法に関する研究.” 2017. Web. 24 Jan 2021.

Vancouver:

Yamaguchi K. On Asteroid Deflection Techniques Exploiting Space Plasma Environment : 宇宙プラズマ環境を利用した小惑星の軌道変更手法に関する研究. [Internet] [Thesis]. Kyoto University / 京都大学; 2017. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/2433/225600 ; http://dx.doi.org/10.14989/doctor.k20375.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Yamaguchi K. On Asteroid Deflection Techniques Exploiting Space Plasma Environment : 宇宙プラズマ環境を利用した小惑星の軌道変更手法に関する研究. [Thesis]. Kyoto University / 京都大学; 2017. Available from: http://hdl.handle.net/2433/225600 ; http://dx.doi.org/10.14989/doctor.k20375

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

26. Yamaguchi, Kouhei. On Asteroid Deflection Techniques Exploiting Space Plasma Environment .

Degree: 2017, Kyoto University

Subjects/Keywords: Asteroid deflection missions; Electric solar wind sail; Coulomb force attractor; Spacecraft charging; Kinetic impactor

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APA (6th Edition):

Yamaguchi, K. (2017). On Asteroid Deflection Techniques Exploiting Space Plasma Environment . (Thesis). Kyoto University. Retrieved from http://hdl.handle.net/2433/225600

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Yamaguchi, Kouhei. “On Asteroid Deflection Techniques Exploiting Space Plasma Environment .” 2017. Thesis, Kyoto University. Accessed January 24, 2021. http://hdl.handle.net/2433/225600.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Yamaguchi, Kouhei. “On Asteroid Deflection Techniques Exploiting Space Plasma Environment .” 2017. Web. 24 Jan 2021.

Vancouver:

Yamaguchi K. On Asteroid Deflection Techniques Exploiting Space Plasma Environment . [Internet] [Thesis]. Kyoto University; 2017. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/2433/225600.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Yamaguchi K. On Asteroid Deflection Techniques Exploiting Space Plasma Environment . [Thesis]. Kyoto University; 2017. Available from: http://hdl.handle.net/2433/225600

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

27. Ramon, Roger Gutierrez. Model for Touchdown Dynamics of a Lander on the Solar Power Sail Mission.

Degree: Electrical and Space Engineering, 2016, Luleå University of Technology

  The ISAS/JAXA Solar Power Sail mission, bound to explore the Jupiter trojans, will face many challenges during its journey. The landing manoeuvre is one… (more)

Subjects/Keywords: ISAS; JAXA; Lander; Solar Sail; Touchdown Dynamics; Jupiter trojans; Aerospace Engineering; Rymd- och flygteknik

solar sail of the IKAROS spacecraft seen from one of the deployable cameras. Mission sequence… …IKAROS solar sail (front right) and the new solar sail (back)… …Point of departure parameters for the Solar Power Sail lander… …SRP Smart Lander for Investigation Moon Solar Power Sail Solar Radiation Pressure VLBI… …successful interplanetary Solar Power Sail (SPS) technology demonstration in the world… 

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APA (6th Edition):

Ramon, R. G. (2016). Model for Touchdown Dynamics of a Lander on the Solar Power Sail Mission. (Thesis). Luleå University of Technology. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-60501

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Ramon, Roger Gutierrez. “Model for Touchdown Dynamics of a Lander on the Solar Power Sail Mission.” 2016. Thesis, Luleå University of Technology. Accessed January 24, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-60501.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Ramon, Roger Gutierrez. “Model for Touchdown Dynamics of a Lander on the Solar Power Sail Mission.” 2016. Web. 24 Jan 2021.

Vancouver:

Ramon RG. Model for Touchdown Dynamics of a Lander on the Solar Power Sail Mission. [Internet] [Thesis]. Luleå University of Technology; 2016. [cited 2021 Jan 24]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-60501.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Ramon RG. Model for Touchdown Dynamics of a Lander on the Solar Power Sail Mission. [Thesis]. Luleå University of Technology; 2016. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-60501

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

28. Karwas, Alex A. An Unconditionally Stable Method for Numerically Solving Solar Sail Spacecraft Equations of Motion.

Degree: PhD, Aerospace Engineering, 2015, University of Kansas

Solar sails use the endless supply of the Sun's radiation to propel spacecraft through space. The sails use the momentum transfer from the impinging solar(more)

Subjects/Keywords: Aerospace engineering; Finite Element Method; Propagation; Sailcraft; Solar Sail; Spacecraft; Trajectory

…10 Figure 1.5 Summary of Solar Sail Research… …research topic, which includes the motivation of the research, brief details of solar sail… …research and the purpose for conducting the research. 1.1.1 Motivation Solar sail spacecraft… …sailcraft EOM will help increase the success rate of solar sail missions. It will help by… …producing thrust and providing attitude control for the sailcraft. The next solar sail spacecraft… 

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

APA (6th Edition):

Karwas, A. A. (2015). An Unconditionally Stable Method for Numerically Solving Solar Sail Spacecraft Equations of Motion. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/19374

Chicago Manual of Style (16th Edition):

Karwas, Alex A. “An Unconditionally Stable Method for Numerically Solving Solar Sail Spacecraft Equations of Motion.” 2015. Doctoral Dissertation, University of Kansas. Accessed January 24, 2021. http://hdl.handle.net/1808/19374.

MLA Handbook (7th Edition):

Karwas, Alex A. “An Unconditionally Stable Method for Numerically Solving Solar Sail Spacecraft Equations of Motion.” 2015. Web. 24 Jan 2021.

Vancouver:

Karwas AA. An Unconditionally Stable Method for Numerically Solving Solar Sail Spacecraft Equations of Motion. [Internet] [Doctoral dissertation]. University of Kansas; 2015. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/1808/19374.

Council of Science Editors:

Karwas AA. An Unconditionally Stable Method for Numerically Solving Solar Sail Spacecraft Equations of Motion. [Doctoral Dissertation]. University of Kansas; 2015. Available from: http://hdl.handle.net/1808/19374


York University

29. Mungo, Mark Julian Adam. Emergence.

Degree: MFA - Master of Fine Arts, Film And Video, 2020, York University

 Emergence is a feature-length coming-of-age and science-fiction screenplay set between 2044 and 2059 in Canada and a settlement on Mars. The story follows Nate Ein,… (more)

Subjects/Keywords: Philosophy of science; Screenwriting; Screenplay; Script; Fiction; Science Fiction; Sci-fi; Coming of age; Coming-of-age; Emergence; Mosaic; Mosaicism; Mosaicist; Futurism; Futurist; Marxism; Marxist; Utopia; Utopian; Epistemology; Social Epistemology; Civilization; Capitalism; Imperialism; Corporate; Treeconomics; UN; Sanctum; Automation; Artificial Intelligence; AI; A.I.; Space Elevator; Solar Sail; 3d Printing; 3d Printers; Neural Interface; Brain Interface; Virtual Reality; Simulations; Global Command; Immortality; Collective; Collective Consciousness; Hive Mind; Group Mind; Decision-making; Themes; Spectrums; Contradictions; Power; Balance; Trust; Choice

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

APA (6th Edition):

Mungo, M. J. A. (2020). Emergence. (Masters Thesis). York University. Retrieved from http://hdl.handle.net/10315/38005

Chicago Manual of Style (16th Edition):

Mungo, Mark Julian Adam. “Emergence.” 2020. Masters Thesis, York University. Accessed January 24, 2021. http://hdl.handle.net/10315/38005.

MLA Handbook (7th Edition):

Mungo, Mark Julian Adam. “Emergence.” 2020. Web. 24 Jan 2021.

Vancouver:

Mungo MJA. Emergence. [Internet] [Masters thesis]. York University; 2020. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/10315/38005.

Council of Science Editors:

Mungo MJA. Emergence. [Masters Thesis]. York University; 2020. Available from: http://hdl.handle.net/10315/38005

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