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137 total matches.

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- 2017 – 2021 (55)
- 2012 – 2016 (59)
- 2007 – 2011 (21)

Universities

- Cal Poly (37)
- Delft University of Technology (21)
- University of Colorado (17)
- Penn State University (12)

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Embry-Riddle Aeronautical University

1. Iyengar, Spatika Dasharati. Computation of Hypersonic Flows with Lateral Jets Using k-ω Turbulence Model.

Degree: MSin Aerospace Engineering, Graduate Studies, 2015, Embry-Riddle Aeronautical University

URL: https://commons.erau.edu/edt/251

► Thermal Protection systems (TPS) are used as shields in space vehicles which encounter high heat and temperatures at the reentry altitudes. Among them, the…
(more)

Subjects/Keywords: Astrodynamics

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

APA (6^{th} Edition):

Iyengar, S. D. (2015). Computation of Hypersonic Flows with Lateral Jets Using k-ω Turbulence Model. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/251

Chicago Manual of Style (16^{th} Edition):

Iyengar, Spatika Dasharati. “Computation of Hypersonic Flows with Lateral Jets Using k-ω Turbulence Model.” 2015. Masters Thesis, Embry-Riddle Aeronautical University. Accessed March 07, 2021. https://commons.erau.edu/edt/251.

MLA Handbook (7^{th} Edition):

Iyengar, Spatika Dasharati. “Computation of Hypersonic Flows with Lateral Jets Using k-ω Turbulence Model.” 2015. Web. 07 Mar 2021.

Vancouver:

Iyengar SD. Computation of Hypersonic Flows with Lateral Jets Using k-ω Turbulence Model. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2015. [cited 2021 Mar 07]. Available from: https://commons.erau.edu/edt/251.

Council of Science Editors:

Iyengar SD. Computation of Hypersonic Flows with Lateral Jets Using k-ω Turbulence Model. [Masters Thesis]. Embry-Riddle Aeronautical University; 2015. Available from: https://commons.erau.edu/edt/251

2.
Vittaldev, V. (author).
The Unified State Model. Derivation and Applications in *Astrodynamics* and Navigation.

Degree: 2010, Delft University of Technology

URL: http://resolver.tudelft.nl/uuid:198390b8-b81f-4a13-9c80-15befd3c0428

Astrodynamics and Space Missions

Aerospace Engineering

Subjects/Keywords: Astrodynamics

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4 *Astrodynamics* and Orbital Mechanics
4.1 Gravity… …of *astrodynamics* and the space
environment with the various perturbations…

Record Details Similar Records

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APA (6^{th} Edition):

Vittaldev, V. (. (2010). The Unified State Model. Derivation and Applications in Astrodynamics and Navigation. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:198390b8-b81f-4a13-9c80-15befd3c0428

Chicago Manual of Style (16^{th} Edition):

Vittaldev, V (author). “The Unified State Model. Derivation and Applications in Astrodynamics and Navigation.” 2010. Masters Thesis, Delft University of Technology. Accessed March 07, 2021. http://resolver.tudelft.nl/uuid:198390b8-b81f-4a13-9c80-15befd3c0428.

MLA Handbook (7^{th} Edition):

Vittaldev, V (author). “The Unified State Model. Derivation and Applications in Astrodynamics and Navigation.” 2010. Web. 07 Mar 2021.

Vancouver:

Vittaldev V(. The Unified State Model. Derivation and Applications in Astrodynamics and Navigation. [Internet] [Masters thesis]. Delft University of Technology; 2010. [cited 2021 Mar 07]. Available from: http://resolver.tudelft.nl/uuid:198390b8-b81f-4a13-9c80-15befd3c0428.

Council of Science Editors:

Vittaldev V(. The Unified State Model. Derivation and Applications in Astrodynamics and Navigation. [Masters Thesis]. Delft University of Technology; 2010. Available from: http://resolver.tudelft.nl/uuid:198390b8-b81f-4a13-9c80-15befd3c0428

Embry-Riddle Aeronautical University

3. Sestak, Timothy Allen. The Effect of Surface Materials and Morphology on Wingsuit Aerodynamics.

Degree: PhD, College of Aviation, 2017, Embry-Riddle Aeronautical University

URL: https://commons.erau.edu/edt/355

► This study examines the aerodynamic effects of the materials, textiles, and morphologies currently used in wingsuit design and construction. The experiment was a low-speed…
(more)

Subjects/Keywords: Astrodynamics; Aviation

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APA (6^{th} Edition):

Sestak, T. A. (2017). The Effect of Surface Materials and Morphology on Wingsuit Aerodynamics. (Doctoral Dissertation). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/355

Chicago Manual of Style (16^{th} Edition):

Sestak, Timothy Allen. “The Effect of Surface Materials and Morphology on Wingsuit Aerodynamics.” 2017. Doctoral Dissertation, Embry-Riddle Aeronautical University. Accessed March 07, 2021. https://commons.erau.edu/edt/355.

MLA Handbook (7^{th} Edition):

Sestak, Timothy Allen. “The Effect of Surface Materials and Morphology on Wingsuit Aerodynamics.” 2017. Web. 07 Mar 2021.

Vancouver:

Sestak TA. The Effect of Surface Materials and Morphology on Wingsuit Aerodynamics. [Internet] [Doctoral dissertation]. Embry-Riddle Aeronautical University; 2017. [cited 2021 Mar 07]. Available from: https://commons.erau.edu/edt/355.

Council of Science Editors:

Sestak TA. The Effect of Surface Materials and Morphology on Wingsuit Aerodynamics. [Doctoral Dissertation]. Embry-Riddle Aeronautical University; 2017. Available from: https://commons.erau.edu/edt/355

University of Florida

4. Kelly, Patrick W. Orbital Debris Mitigation Using Solar Sail Trajectory Optimization.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2018, University of Florida

URL: https://ufdc.ufl.edu/UFE0053995

► Solar-sailing satellites offer unique propulsive advantages for orbit manipulation and propellant mass requirements. When compared with traditional, propellant-based satellites, solar-sailing spacecraft are not limited by…
(more)

Subjects/Keywords: astrodynamics – optimization

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APA (6^{th} Edition):

Kelly, P. W. (2018). Orbital Debris Mitigation Using Solar Sail Trajectory Optimization. (Doctoral Dissertation). University of Florida. Retrieved from https://ufdc.ufl.edu/UFE0053995

Chicago Manual of Style (16^{th} Edition):

Kelly, Patrick W. “Orbital Debris Mitigation Using Solar Sail Trajectory Optimization.” 2018. Doctoral Dissertation, University of Florida. Accessed March 07, 2021. https://ufdc.ufl.edu/UFE0053995.

MLA Handbook (7^{th} Edition):

Kelly, Patrick W. “Orbital Debris Mitigation Using Solar Sail Trajectory Optimization.” 2018. Web. 07 Mar 2021.

Vancouver:

Kelly PW. Orbital Debris Mitigation Using Solar Sail Trajectory Optimization. [Internet] [Doctoral dissertation]. University of Florida; 2018. [cited 2021 Mar 07]. Available from: https://ufdc.ufl.edu/UFE0053995.

Council of Science Editors:

Kelly PW. Orbital Debris Mitigation Using Solar Sail Trajectory Optimization. [Doctoral Dissertation]. University of Florida; 2018. Available from: https://ufdc.ufl.edu/UFE0053995

Cal Poly

5. Farahmand, Mitra. ORBITAL PROPAGATORS FOR HORIZON SIMULATION FRAMEWORK.

Degree: MS, Aerospace Engineering, 2009, Cal Poly

URL: https://digitalcommons.calpoly.edu/theses/167 ; 10.15368/theses.2009.138

► This thesis describes the models of four common orbital propagators and outlines the process of integrating them into the Horizon Simulation Framework (HSF). The results…
(more)

Subjects/Keywords: Astrodynamics

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APA (6^{th} Edition):

Farahmand, M. (2009). ORBITAL PROPAGATORS FOR HORIZON SIMULATION FRAMEWORK. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/167 ; 10.15368/theses.2009.138

Chicago Manual of Style (16^{th} Edition):

Farahmand, Mitra. “ORBITAL PROPAGATORS FOR HORIZON SIMULATION FRAMEWORK.” 2009. Masters Thesis, Cal Poly. Accessed March 07, 2021. https://digitalcommons.calpoly.edu/theses/167 ; 10.15368/theses.2009.138.

MLA Handbook (7^{th} Edition):

Farahmand, Mitra. “ORBITAL PROPAGATORS FOR HORIZON SIMULATION FRAMEWORK.” 2009. Web. 07 Mar 2021.

Vancouver:

Farahmand M. ORBITAL PROPAGATORS FOR HORIZON SIMULATION FRAMEWORK. [Internet] [Masters thesis]. Cal Poly; 2009. [cited 2021 Mar 07]. Available from: https://digitalcommons.calpoly.edu/theses/167 ; 10.15368/theses.2009.138.

Council of Science Editors:

Farahmand M. ORBITAL PROPAGATORS FOR HORIZON SIMULATION FRAMEWORK. [Masters Thesis]. Cal Poly; 2009. Available from: https://digitalcommons.calpoly.edu/theses/167 ; 10.15368/theses.2009.138

Purdue University

6. Haapala, Amanda F. Trajectory design in the spatial circular restricted three-body problem exploiting higher-dimensional Poincare maps.

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

URL: https://docs.lib.purdue.edu/open_access_dissertations/278

► In this investigation, the role of higher-dimensional Poincaré maps in facilitating trajectory design is explored for a variety of applications. To begin, existing strategies…
(more)

Subjects/Keywords: Aerospace Engineering; Astrodynamics

Record Details Similar Records

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APA (6^{th} Edition):

Haapala, A. F. (2014). Trajectory design in the spatial circular restricted three-body problem exploiting higher-dimensional Poincare maps. (Doctoral Dissertation). Purdue University. Retrieved from https://docs.lib.purdue.edu/open_access_dissertations/278

Chicago Manual of Style (16^{th} Edition):

Haapala, Amanda F. “Trajectory design in the spatial circular restricted three-body problem exploiting higher-dimensional Poincare maps.” 2014. Doctoral Dissertation, Purdue University. Accessed March 07, 2021. https://docs.lib.purdue.edu/open_access_dissertations/278.

MLA Handbook (7^{th} Edition):

Haapala, Amanda F. “Trajectory design in the spatial circular restricted three-body problem exploiting higher-dimensional Poincare maps.” 2014. Web. 07 Mar 2021.

Vancouver:

Haapala AF. Trajectory design in the spatial circular restricted three-body problem exploiting higher-dimensional Poincare maps. [Internet] [Doctoral dissertation]. Purdue University; 2014. [cited 2021 Mar 07]. Available from: https://docs.lib.purdue.edu/open_access_dissertations/278.

Council of Science Editors:

Haapala AF. Trajectory design in the spatial circular restricted three-body problem exploiting higher-dimensional Poincare maps. [Doctoral Dissertation]. Purdue University; 2014. Available from: https://docs.lib.purdue.edu/open_access_dissertations/278

Penn State University

7. Conte, Davide. Determination of Optimal Earth-mars Trajectories to Target the Moons of Mars.

Degree: 2014, Penn State University

URL: https://submit-etda.libraries.psu.edu/catalog/21382

► The focus of this thesis is to analyze interplanetary transfer maneuvers from Earth to Mars in order to target the Martian moons, Phobos and Deimos.…
(more)

Subjects/Keywords: Mars; Phobos; Deimos; astrodynamics

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APA (6^{th} Edition):

Conte, D. (2014). Determination of Optimal Earth-mars Trajectories to Target the Moons of Mars. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/21382

Note: this citation may be lacking information needed for this citation format:

Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^{th} Edition):

Conte, Davide. “Determination of Optimal Earth-mars Trajectories to Target the Moons of Mars.” 2014. Thesis, Penn State University. Accessed March 07, 2021. https://submit-etda.libraries.psu.edu/catalog/21382.

Note: this citation may be lacking information needed for this citation format:

Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^{th} Edition):

Conte, Davide. “Determination of Optimal Earth-mars Trajectories to Target the Moons of Mars.” 2014. Web. 07 Mar 2021.

Vancouver:

Conte D. Determination of Optimal Earth-mars Trajectories to Target the Moons of Mars. [Internet] [Thesis]. Penn State University; 2014. [cited 2021 Mar 07]. Available from: https://submit-etda.libraries.psu.edu/catalog/21382.

Note: this citation may be lacking information needed for this citation format:

Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Conte D. Determination of Optimal Earth-mars Trajectories to Target the Moons of Mars. [Thesis]. Penn State University; 2014. Available from: https://submit-etda.libraries.psu.edu/catalog/21382

Not specified: Masters Thesis or Doctoral Dissertation

Embry-Riddle Aeronautical University

8. Coulter, Nolan. Design of an Attitude Control System for a Spacecraft with Propellant Slosh Dynamics.

Degree: MSin Aerospace Engineering, Graduate Studies, 2018, Embry-Riddle Aeronautical University

URL: https://commons.erau.edu/edt/424

► The presence of propellant slosh dynamics in a spacecraft system during a maneuver leads to attitude control system (ACS) performance degradation resulting in attitude…
(more)

Subjects/Keywords: Aerospace Engineering; Astrodynamics; Space Vehicles

Record Details Similar Records

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APA (6^{th} Edition):

Coulter, N. (2018). Design of an Attitude Control System for a Spacecraft with Propellant Slosh Dynamics. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/424

Chicago Manual of Style (16^{th} Edition):

Coulter, Nolan. “Design of an Attitude Control System for a Spacecraft with Propellant Slosh Dynamics.” 2018. Masters Thesis, Embry-Riddle Aeronautical University. Accessed March 07, 2021. https://commons.erau.edu/edt/424.

MLA Handbook (7^{th} Edition):

Coulter, Nolan. “Design of an Attitude Control System for a Spacecraft with Propellant Slosh Dynamics.” 2018. Web. 07 Mar 2021.

Vancouver:

Coulter N. Design of an Attitude Control System for a Spacecraft with Propellant Slosh Dynamics. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2018. [cited 2021 Mar 07]. Available from: https://commons.erau.edu/edt/424.

Council of Science Editors:

Coulter N. Design of an Attitude Control System for a Spacecraft with Propellant Slosh Dynamics. [Masters Thesis]. Embry-Riddle Aeronautical University; 2018. Available from: https://commons.erau.edu/edt/424

Delft University of Technology

9. Agrawal, Abhishek (author). Orbital motion of regolith around asteroids.

Degree: 2018, Delft University of Technology

URL: http://resolver.tudelft.nl/uuid:0933c1e6-89ee-476c-9b45-3e6d235ddac6

► We study the orbital motion of regolith around asteroids, lofted from the surface due to impact cratering events, to understand the displacement of material on…
(more)

Subjects/Keywords: Astrodynamics; Regolith; Asteroids; Numerical Simulation

Record Details Similar Records

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APA (6^{th} Edition):

Agrawal, A. (. (2018). Orbital motion of regolith around asteroids. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:0933c1e6-89ee-476c-9b45-3e6d235ddac6

Chicago Manual of Style (16^{th} Edition):

Agrawal, Abhishek (author). “Orbital motion of regolith around asteroids.” 2018. Masters Thesis, Delft University of Technology. Accessed March 07, 2021. http://resolver.tudelft.nl/uuid:0933c1e6-89ee-476c-9b45-3e6d235ddac6.

MLA Handbook (7^{th} Edition):

Agrawal, Abhishek (author). “Orbital motion of regolith around asteroids.” 2018. Web. 07 Mar 2021.

Vancouver:

Agrawal A(. Orbital motion of regolith around asteroids. [Internet] [Masters thesis]. Delft University of Technology; 2018. [cited 2021 Mar 07]. Available from: http://resolver.tudelft.nl/uuid:0933c1e6-89ee-476c-9b45-3e6d235ddac6.

Council of Science Editors:

Agrawal A(. Orbital motion of regolith around asteroids. [Masters Thesis]. Delft University of Technology; 2018. Available from: http://resolver.tudelft.nl/uuid:0933c1e6-89ee-476c-9b45-3e6d235ddac6

Delft University of Technology

10. de Jong, Hanneke (author). Analytical Low-Thrust Trajectory Design: Using the Simplified General Perturbations Model.

Degree: 2018, Delft University of Technology

URL: http://resolver.tudelft.nl/uuid:1c58ca05-b367-48e6-9b4c-e31f12f488d7

►

An analytical low-thrust design tool for orbits around Earth has been developed which takes perturbations into account. The Simplified General Perturbations 4 model (SGP4) is… (more)

Subjects/Keywords: astrodynamics; SGP4; Low-thrust

Record Details Similar Records

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APA (6^{th} Edition):

de Jong, H. (. (2018). Analytical Low-Thrust Trajectory Design: Using the Simplified General Perturbations Model. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:1c58ca05-b367-48e6-9b4c-e31f12f488d7

Chicago Manual of Style (16^{th} Edition):

de Jong, Hanneke (author). “Analytical Low-Thrust Trajectory Design: Using the Simplified General Perturbations Model.” 2018. Masters Thesis, Delft University of Technology. Accessed March 07, 2021. http://resolver.tudelft.nl/uuid:1c58ca05-b367-48e6-9b4c-e31f12f488d7.

MLA Handbook (7^{th} Edition):

de Jong, Hanneke (author). “Analytical Low-Thrust Trajectory Design: Using the Simplified General Perturbations Model.” 2018. Web. 07 Mar 2021.

Vancouver:

de Jong H(. Analytical Low-Thrust Trajectory Design: Using the Simplified General Perturbations Model. [Internet] [Masters thesis]. Delft University of Technology; 2018. [cited 2021 Mar 07]. Available from: http://resolver.tudelft.nl/uuid:1c58ca05-b367-48e6-9b4c-e31f12f488d7.

Council of Science Editors:

de Jong H(. Analytical Low-Thrust Trajectory Design: Using the Simplified General Perturbations Model. [Masters Thesis]. Delft University of Technology; 2018. Available from: http://resolver.tudelft.nl/uuid:1c58ca05-b367-48e6-9b4c-e31f12f488d7

University of Illinois – Urbana-Champaign

11. Ponnapalli, Kaushik. Optimal variable-specific-impulse trajectories in simple gravitational fields.

Degree: MS, Aerospace Engineering, 2019, University of Illinois – Urbana-Champaign

URL: http://hdl.handle.net/2142/104920

► Minimum-fuel trajectories in the Clohessy-Wiltshire orbital model are investigated. Low-thrust variable-speciﬁc-impulse propulsion is assumed. The necessary conditions for an optimal solution and the equations of…
(more)

Subjects/Keywords: Astrodynamics, Optimal Trajectories; Trajectory Optimization

Record Details Similar Records

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APA (6^{th} Edition):

Ponnapalli, K. (2019). Optimal variable-specific-impulse trajectories in simple gravitational fields. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/104920

Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^{th} Edition):

Ponnapalli, Kaushik. “Optimal variable-specific-impulse trajectories in simple gravitational fields.” 2019. Thesis, University of Illinois – Urbana-Champaign. Accessed March 07, 2021. http://hdl.handle.net/2142/104920.

Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^{th} Edition):

Ponnapalli, Kaushik. “Optimal variable-specific-impulse trajectories in simple gravitational fields.” 2019. Web. 07 Mar 2021.

Vancouver:

Ponnapalli K. Optimal variable-specific-impulse trajectories in simple gravitational fields. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2019. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/2142/104920.

Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Ponnapalli K. Optimal variable-specific-impulse trajectories in simple gravitational fields. [Thesis]. University of Illinois – Urbana-Champaign; 2019. Available from: http://hdl.handle.net/2142/104920

Not specified: Masters Thesis or Doctoral Dissertation

University of New South Wales

12. Crowe, William. Use of Spacecraft Swarms to Characterise Asteroids during Flyby.

Degree: Mechanical & Manufacturing Engineering, 2018, University of New South Wales

URL: http://handle.unsw.edu.au/1959.4/60892

► Of the more than 700,000 asteroids known today, only 12 have been visited by spacecraft. This means that many assumptions about their characteristics remain unverified.…
(more)

Subjects/Keywords: Spacecraft; Asteroids; Astrodynamics; Swarms

Record Details Similar Records

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APA (6^{th} Edition):

Crowe, W. (2018). Use of Spacecraft Swarms to Characterise Asteroids during Flyby. (Doctoral Dissertation). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/60892

Chicago Manual of Style (16^{th} Edition):

Crowe, William. “Use of Spacecraft Swarms to Characterise Asteroids during Flyby.” 2018. Doctoral Dissertation, University of New South Wales. Accessed March 07, 2021. http://handle.unsw.edu.au/1959.4/60892.

MLA Handbook (7^{th} Edition):

Crowe, William. “Use of Spacecraft Swarms to Characterise Asteroids during Flyby.” 2018. Web. 07 Mar 2021.

Vancouver:

Crowe W. Use of Spacecraft Swarms to Characterise Asteroids during Flyby. [Internet] [Doctoral dissertation]. University of New South Wales; 2018. [cited 2021 Mar 07]. Available from: http://handle.unsw.edu.au/1959.4/60892.

Council of Science Editors:

Crowe W. Use of Spacecraft Swarms to Characterise Asteroids during Flyby. [Doctoral Dissertation]. University of New South Wales; 2018. Available from: http://handle.unsw.edu.au/1959.4/60892

Delft University of Technology

13. Vandenberghe, Alexander (author). Station-keeping in the vicinity of the collinear Lagrange points.

Degree: 2020, Delft University of Technology

URL: http://resolver.tudelft.nl/uuid:8b82e473-2ed1-48c4-ac3e-a59ee1a5039c

►

In this thesis, the performance of three different station-keeping methods applied to Sun-Earth L2 halo orbits is investigated. In order to evaluate these methods, first… (more)

Subjects/Keywords: Station-keeping; Halo; Astrodynamics; Optimisation

Record Details Similar Records

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

APA (6^{th} Edition):

Vandenberghe, A. (. (2020). Station-keeping in the vicinity of the collinear Lagrange points. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:8b82e473-2ed1-48c4-ac3e-a59ee1a5039c

Chicago Manual of Style (16^{th} Edition):

Vandenberghe, Alexander (author). “Station-keeping in the vicinity of the collinear Lagrange points.” 2020. Masters Thesis, Delft University of Technology. Accessed March 07, 2021. http://resolver.tudelft.nl/uuid:8b82e473-2ed1-48c4-ac3e-a59ee1a5039c.

MLA Handbook (7^{th} Edition):

Vandenberghe, Alexander (author). “Station-keeping in the vicinity of the collinear Lagrange points.” 2020. Web. 07 Mar 2021.

Vancouver:

Vandenberghe A(. Station-keeping in the vicinity of the collinear Lagrange points. [Internet] [Masters thesis]. Delft University of Technology; 2020. [cited 2021 Mar 07]. Available from: http://resolver.tudelft.nl/uuid:8b82e473-2ed1-48c4-ac3e-a59ee1a5039c.

Council of Science Editors:

Vandenberghe A(. Station-keeping in the vicinity of the collinear Lagrange points. [Masters Thesis]. Delft University of Technology; 2020. Available from: http://resolver.tudelft.nl/uuid:8b82e473-2ed1-48c4-ac3e-a59ee1a5039c

Cal Poly

14. Graef, Jared. B-Plane Targeting with the Spacecraft Trajectory Optimization Suite.

Degree: MS, Aerospace Engineering, 2020, Cal Poly

URL: https://digitalcommons.calpoly.edu/theses/2251

► In interplanetary trajectory applications, it is common to design arrival trajectories based on B-plane target values. This targeting scheme, B-plane targeting, allows for specific…
(more)

Subjects/Keywords: Optimization; Astrodynamics; B-Plane Targeting; Interplanetary; Astrodynamics; Space Vehicles

Record Details Similar Records

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APA (6^{th} Edition):

Graef, J. (2020). B-Plane Targeting with the Spacecraft Trajectory Optimization Suite. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/2251

Chicago Manual of Style (16^{th} Edition):

Graef, Jared. “B-Plane Targeting with the Spacecraft Trajectory Optimization Suite.” 2020. Masters Thesis, Cal Poly. Accessed March 07, 2021. https://digitalcommons.calpoly.edu/theses/2251.

MLA Handbook (7^{th} Edition):

Graef, Jared. “B-Plane Targeting with the Spacecraft Trajectory Optimization Suite.” 2020. Web. 07 Mar 2021.

Vancouver:

Graef J. B-Plane Targeting with the Spacecraft Trajectory Optimization Suite. [Internet] [Masters thesis]. Cal Poly; 2020. [cited 2021 Mar 07]. Available from: https://digitalcommons.calpoly.edu/theses/2251.

Council of Science Editors:

Graef J. B-Plane Targeting with the Spacecraft Trajectory Optimization Suite. [Masters Thesis]. Cal Poly; 2020. Available from: https://digitalcommons.calpoly.edu/theses/2251

University of Colorado

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

Degree: PhD, 2017, University of Colorado

URL: https://scholar.colorado.edu/asen_gradetds/192

► 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

Record Details Similar Records

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

APA (6^{th} 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 (16^{th} Edition):

Geeraert, Jeroen L. “Multi-Satellite Orbit Determination Using Interferometric Observables with RF Localization Applications.” 2017. Doctoral Dissertation, University of Colorado. Accessed March 07, 2021. https://scholar.colorado.edu/asen_gradetds/192.

MLA Handbook (7^{th} Edition):

Geeraert, Jeroen L. “Multi-Satellite Orbit Determination Using Interferometric Observables with RF Localization Applications.” 2017. Web. 07 Mar 2021.

Vancouver:

Geeraert JL. Multi-Satellite Orbit Determination Using Interferometric Observables with RF Localization Applications. [Internet] [Doctoral dissertation]. University of Colorado; 2017. [cited 2021 Mar 07]. 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

Delft University of Technology

16. Villegas Pinto, Daniel (author). Temporary Capture of Asteroid Ejecta into Periodic Orbits: Application to JAXA’s Hayabusa2 Impact Event.

Degree: 2019, Delft University of Technology

URL: http://resolver.tudelft.nl/uuid:d9768a7f-0c57-4437-befb-4ccf7a39a0a5

► In the framework of JAXA’s Hayabusa2 mission, we study the dynamical environment around asteroid Ryugu to investigate whether ejecta particles can be temporarily trapped in…
(more)

Subjects/Keywords: Augmented Hill Problem; Astrodynamics; Asteroid Ejecta

Record Details Similar Records

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APA (6^{th} Edition):

Villegas Pinto, D. (. (2019). Temporary Capture of Asteroid Ejecta into Periodic Orbits: Application to JAXA’s Hayabusa2 Impact Event. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:d9768a7f-0c57-4437-befb-4ccf7a39a0a5

Chicago Manual of Style (16^{th} Edition):

Villegas Pinto, Daniel (author). “Temporary Capture of Asteroid Ejecta into Periodic Orbits: Application to JAXA’s Hayabusa2 Impact Event.” 2019. Masters Thesis, Delft University of Technology. Accessed March 07, 2021. http://resolver.tudelft.nl/uuid:d9768a7f-0c57-4437-befb-4ccf7a39a0a5.

MLA Handbook (7^{th} Edition):

Villegas Pinto, Daniel (author). “Temporary Capture of Asteroid Ejecta into Periodic Orbits: Application to JAXA’s Hayabusa2 Impact Event.” 2019. Web. 07 Mar 2021.

Vancouver:

Villegas Pinto D(. Temporary Capture of Asteroid Ejecta into Periodic Orbits: Application to JAXA’s Hayabusa2 Impact Event. [Internet] [Masters thesis]. Delft University of Technology; 2019. [cited 2021 Mar 07]. Available from: http://resolver.tudelft.nl/uuid:d9768a7f-0c57-4437-befb-4ccf7a39a0a5.

Council of Science Editors:

Villegas Pinto D(. Temporary Capture of Asteroid Ejecta into Periodic Orbits: Application to JAXA’s Hayabusa2 Impact Event. [Masters Thesis]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:d9768a7f-0c57-4437-befb-4ccf7a39a0a5

Delft University of Technology

17. Hess, J.R. (author). Aerogravity assists: Hypersonic maneuvering to improve planetary gravity assists.

Degree: 2016, Delft University of Technology

URL: http://resolver.tudelft.nl/uuid:dee2d842-ca91-4086-8ef8-771cfee1b0dc

► Interplanetary missions use gravitational slingshots around planetary bodies to adjust their heliocentric velocity or inclination for quite some time. The momentum exchange that can be…
(more)

Subjects/Keywords: astrodynamics; aerogravity; gravity; assist; optimization; hypersonics; waverider

Record Details Similar Records

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APA (6^{th} Edition):

Hess, J. R. (. (2016). Aerogravity assists: Hypersonic maneuvering to improve planetary gravity assists. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:dee2d842-ca91-4086-8ef8-771cfee1b0dc

Chicago Manual of Style (16^{th} Edition):

Hess, J R (author). “Aerogravity assists: Hypersonic maneuvering to improve planetary gravity assists.” 2016. Masters Thesis, Delft University of Technology. Accessed March 07, 2021. http://resolver.tudelft.nl/uuid:dee2d842-ca91-4086-8ef8-771cfee1b0dc.

MLA Handbook (7^{th} Edition):

Hess, J R (author). “Aerogravity assists: Hypersonic maneuvering to improve planetary gravity assists.” 2016. Web. 07 Mar 2021.

Vancouver:

Hess JR(. Aerogravity assists: Hypersonic maneuvering to improve planetary gravity assists. [Internet] [Masters thesis]. Delft University of Technology; 2016. [cited 2021 Mar 07]. Available from: http://resolver.tudelft.nl/uuid:dee2d842-ca91-4086-8ef8-771cfee1b0dc.

Council of Science Editors:

Hess JR(. Aerogravity assists: Hypersonic maneuvering to improve planetary gravity assists. [Masters Thesis]. Delft University of Technology; 2016. Available from: http://resolver.tudelft.nl/uuid:dee2d842-ca91-4086-8ef8-771cfee1b0dc

Cal Poly

18. Iuliano, Jay R. A Solution to the Circular Restricted N Body Problem in Planetary Systems.

Degree: MS, Aerospace Engineering, 2016, Cal Poly

URL: https://digitalcommons.calpoly.edu/theses/1612 ; 10.15368/theses.2016.80

► This thesis is a brief look at a new solution to a problem that has been approached in many different ways in the past…
(more)

Subjects/Keywords: Astrodynamics; Navigation, Guidance, Control and Dynamics

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

APA (6^{th} Edition):

Iuliano, J. R. (2016). A Solution to the Circular Restricted N Body Problem in Planetary Systems. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1612 ; 10.15368/theses.2016.80

Chicago Manual of Style (16^{th} Edition):

Iuliano, Jay R. “A Solution to the Circular Restricted N Body Problem in Planetary Systems.” 2016. Masters Thesis, Cal Poly. Accessed March 07, 2021. https://digitalcommons.calpoly.edu/theses/1612 ; 10.15368/theses.2016.80.

MLA Handbook (7^{th} Edition):

Iuliano, Jay R. “A Solution to the Circular Restricted N Body Problem in Planetary Systems.” 2016. Web. 07 Mar 2021.

Vancouver:

Iuliano JR. A Solution to the Circular Restricted N Body Problem in Planetary Systems. [Internet] [Masters thesis]. Cal Poly; 2016. [cited 2021 Mar 07]. Available from: https://digitalcommons.calpoly.edu/theses/1612 ; 10.15368/theses.2016.80.

Council of Science Editors:

Iuliano JR. A Solution to the Circular Restricted N Body Problem in Planetary Systems. [Masters Thesis]. Cal Poly; 2016. Available from: https://digitalcommons.calpoly.edu/theses/1612 ; 10.15368/theses.2016.80

Cal Poly

19. Jackson, Daniel J. Formulation of an Optimal Search Strategy for Space Debris At GEO.

Degree: MS, Aerospace Engineering, 2011, Cal Poly

URL: https://digitalcommons.calpoly.edu/theses/656 ; 10.15368/theses.2011.202

► The purpose of this thesis is to create a search strategy to find orbital debris when the object fails to appear in the sky…
(more)

Subjects/Keywords: aerospace; space; debris; GEO; telescope; MODEST; Astrodynamics

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

APA (6^{th} Edition):

Jackson, D. J. (2011). Formulation of an Optimal Search Strategy for Space Debris At GEO. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/656 ; 10.15368/theses.2011.202

Chicago Manual of Style (16^{th} Edition):

Jackson, Daniel J. “Formulation of an Optimal Search Strategy for Space Debris At GEO.” 2011. Masters Thesis, Cal Poly. Accessed March 07, 2021. https://digitalcommons.calpoly.edu/theses/656 ; 10.15368/theses.2011.202.

MLA Handbook (7^{th} Edition):

Jackson, Daniel J. “Formulation of an Optimal Search Strategy for Space Debris At GEO.” 2011. Web. 07 Mar 2021.

Vancouver:

Jackson DJ. Formulation of an Optimal Search Strategy for Space Debris At GEO. [Internet] [Masters thesis]. Cal Poly; 2011. [cited 2021 Mar 07]. Available from: https://digitalcommons.calpoly.edu/theses/656 ; 10.15368/theses.2011.202.

Council of Science Editors:

Jackson DJ. Formulation of an Optimal Search Strategy for Space Debris At GEO. [Masters Thesis]. Cal Poly; 2011. Available from: https://digitalcommons.calpoly.edu/theses/656 ; 10.15368/theses.2011.202

University of New South Wales

20. Capon, Christopher. Ionospheric Aerodynamics in Low Earth Orbit.

Degree: Engineering & Information Technology, 2017, University of New South Wales

URL: http://handle.unsw.edu.au/1959.4/58652 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:46528/SOURCE01?view=true

► Understanding perturbing forces takes on new significance as the Low Earth Orbit (LEO) environment becomes increasingly congested and the risk of collision events that threaten…
(more)

Subjects/Keywords: Astrodynamics; Ionospheric Aerodynamics; Space Situational Awareness

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APA (6^{th} Edition):

Capon, C. (2017). Ionospheric Aerodynamics in Low Earth Orbit. (Doctoral Dissertation). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/58652 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:46528/SOURCE01?view=true

Chicago Manual of Style (16^{th} Edition):

Capon, Christopher. “Ionospheric Aerodynamics in Low Earth Orbit.” 2017. Doctoral Dissertation, University of New South Wales. Accessed March 07, 2021. http://handle.unsw.edu.au/1959.4/58652 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:46528/SOURCE01?view=true.

MLA Handbook (7^{th} Edition):

Capon, Christopher. “Ionospheric Aerodynamics in Low Earth Orbit.” 2017. Web. 07 Mar 2021.

Vancouver:

Capon C. Ionospheric Aerodynamics in Low Earth Orbit. [Internet] [Doctoral dissertation]. University of New South Wales; 2017. [cited 2021 Mar 07]. Available from: http://handle.unsw.edu.au/1959.4/58652 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:46528/SOURCE01?view=true.

Council of Science Editors:

Capon C. Ionospheric Aerodynamics in Low Earth Orbit. [Doctoral Dissertation]. University of New South Wales; 2017. Available from: http://handle.unsw.edu.au/1959.4/58652 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:46528/SOURCE01?view=true

Delft University of Technology

21. Carvalho Barreira Lages Ribeiro, André (author). Optimal Aeroassisted Maneuvers for Orbital Transfer.

Degree: 2019, Delft University of Technology

URL: http://resolver.tudelft.nl/uuid:89acba76-65ed-438d-810e-f3a863546398

► Orbital plane changes require a considerable amount of propellant to be completed if the traditional fully propulsive maneuver is used. The cost associated with this…
(more)

Subjects/Keywords: Optimization; Re-entry; Aeroassisted; Astrodynamics; Hypersonic

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APA (6^{th} Edition):

Carvalho Barreira Lages Ribeiro, A. (. (2019). Optimal Aeroassisted Maneuvers for Orbital Transfer. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:89acba76-65ed-438d-810e-f3a863546398

Chicago Manual of Style (16^{th} Edition):

Carvalho Barreira Lages Ribeiro, André (author). “Optimal Aeroassisted Maneuvers for Orbital Transfer.” 2019. Masters Thesis, Delft University of Technology. Accessed March 07, 2021. http://resolver.tudelft.nl/uuid:89acba76-65ed-438d-810e-f3a863546398.

MLA Handbook (7^{th} Edition):

Carvalho Barreira Lages Ribeiro, André (author). “Optimal Aeroassisted Maneuvers for Orbital Transfer.” 2019. Web. 07 Mar 2021.

Vancouver:

Carvalho Barreira Lages Ribeiro A(. Optimal Aeroassisted Maneuvers for Orbital Transfer. [Internet] [Masters thesis]. Delft University of Technology; 2019. [cited 2021 Mar 07]. Available from: http://resolver.tudelft.nl/uuid:89acba76-65ed-438d-810e-f3a863546398.

Council of Science Editors:

Carvalho Barreira Lages Ribeiro A(. Optimal Aeroassisted Maneuvers for Orbital Transfer. [Masters Thesis]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:89acba76-65ed-438d-810e-f3a863546398

University of Colorado

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

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

URL: https://scholar.colorado.edu/asen_gradetds/26

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

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

Record Details Similar Records

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

APA (6^{th} Edition):

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

Chicago Manual of Style (16^{th} Edition):

McMahon, Jay Warren. “An Analytical Theory for the Perturbative Effect of Solar Radiation Pressure on Natural and Artificial Satellites.” 2011. Doctoral Dissertation, University of Colorado. Accessed March 07, 2021. https://scholar.colorado.edu/asen_gradetds/26.

MLA Handbook (7^{th} Edition):

McMahon, Jay Warren. “An Analytical Theory for the Perturbative Effect of Solar Radiation Pressure on Natural and Artificial Satellites.” 2011. Web. 07 Mar 2021.

Vancouver:

McMahon JW. An Analytical Theory for the Perturbative Effect of Solar Radiation Pressure on Natural and Artificial Satellites. [Internet] [Doctoral dissertation]. University of Colorado; 2011. [cited 2021 Mar 07]. Available from: https://scholar.colorado.edu/asen_gradetds/26.

Council of Science Editors:

McMahon JW. An Analytical Theory for the Perturbative Effect of Solar Radiation Pressure on Natural and Artificial Satellites. [Doctoral Dissertation]. University of Colorado; 2011. Available from: https://scholar.colorado.edu/asen_gradetds/26

University of Colorado

23. Baresi, Nicola. Spacecraft Formation Flight on Quasi-Periodic Invariant Tori.

Degree: PhD, 2017, University of Colorado

URL: https://scholar.colorado.edu/asen_gradetds/219

► Since the successful rendezvous of the Gemini VI and VII spacecraft in 1965, spacecraft formation flying has attracted the interest of many researchers in…
(more)

Subjects/Keywords: astrodynamics; cluster flight; dynamical systems theory; quasi-periodic invariant tori; spacecraft formation flying; Aerospace Engineering; Astrodynamics

Record Details Similar Records

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

APA (6^{th} Edition):

Baresi, N. (2017). Spacecraft Formation Flight on Quasi-Periodic Invariant Tori. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/219

Chicago Manual of Style (16^{th} Edition):

Baresi, Nicola. “Spacecraft Formation Flight on Quasi-Periodic Invariant Tori.” 2017. Doctoral Dissertation, University of Colorado. Accessed March 07, 2021. https://scholar.colorado.edu/asen_gradetds/219.

MLA Handbook (7^{th} Edition):

Baresi, Nicola. “Spacecraft Formation Flight on Quasi-Periodic Invariant Tori.” 2017. Web. 07 Mar 2021.

Vancouver:

Baresi N. Spacecraft Formation Flight on Quasi-Periodic Invariant Tori. [Internet] [Doctoral dissertation]. University of Colorado; 2017. [cited 2021 Mar 07]. Available from: https://scholar.colorado.edu/asen_gradetds/219.

Council of Science Editors:

Baresi N. Spacecraft Formation Flight on Quasi-Periodic Invariant Tori. [Doctoral Dissertation]. University of Colorado; 2017. Available from: https://scholar.colorado.edu/asen_gradetds/219

University of Colorado

24. De Smet, Stijn. On the Design of Solar Gravity Driven Planetocentric Transfers Using Artificial Neural Networks.

Degree: PhD, 2018, University of Colorado

URL: https://scholar.colorado.edu/asen_gradetds/235

► The sun's gravity can be used to efficiently transfer between different planetocentric orbits. Such transfers cannot be designed in a two-body dynamical system, nor…
(more)

Subjects/Keywords: artificial neural networks; astrodynamics; eccentric hill system; machine learning; periapse poincaré maps; Aerospace Engineering; Astrodynamics; Computer Sciences

Record Details Similar Records

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

APA (6^{th} Edition):

De Smet, S. (2018). On the Design of Solar Gravity Driven Planetocentric Transfers Using Artificial Neural Networks. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/235

Chicago Manual of Style (16^{th} Edition):

De Smet, Stijn. “On the Design of Solar Gravity Driven Planetocentric Transfers Using Artificial Neural Networks.” 2018. Doctoral Dissertation, University of Colorado. Accessed March 07, 2021. https://scholar.colorado.edu/asen_gradetds/235.

MLA Handbook (7^{th} Edition):

De Smet, Stijn. “On the Design of Solar Gravity Driven Planetocentric Transfers Using Artificial Neural Networks.” 2018. Web. 07 Mar 2021.

Vancouver:

De Smet S. On the Design of Solar Gravity Driven Planetocentric Transfers Using Artificial Neural Networks. [Internet] [Doctoral dissertation]. University of Colorado; 2018. [cited 2021 Mar 07]. Available from: https://scholar.colorado.edu/asen_gradetds/235.

Council of Science Editors:

De Smet S. On the Design of Solar Gravity Driven Planetocentric Transfers Using Artificial Neural Networks. [Doctoral Dissertation]. University of Colorado; 2018. Available from: https://scholar.colorado.edu/asen_gradetds/235

Texas A&M University

25. Johnson, Kirk Wayne. Approaches for Modeling Satellite Relative Motion.

Degree: PhD, Aerospace Engineering, 2016, Texas A&M University

URL: http://hdl.handle.net/1969.1/158945

► This dissertation explores new approaches for modeling perturbed and unperturbed satellite relative motion. It extends Hoots orbit theory, an analytical averaging-method perturbation solution to the…
(more)

Subjects/Keywords: Satellite Relative Motion; Satellite Formation Flying; Zonal Problem; Astrodynamics

Record Details Similar Records

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APA (6^{th} Edition):

Johnson, K. W. (2016). Approaches for Modeling Satellite Relative Motion. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/158945

Chicago Manual of Style (16^{th} Edition):

Johnson, Kirk Wayne. “Approaches for Modeling Satellite Relative Motion.” 2016. Doctoral Dissertation, Texas A&M University. Accessed March 07, 2021. http://hdl.handle.net/1969.1/158945.

MLA Handbook (7^{th} Edition):

Johnson, Kirk Wayne. “Approaches for Modeling Satellite Relative Motion.” 2016. Web. 07 Mar 2021.

Vancouver:

Johnson KW. Approaches for Modeling Satellite Relative Motion. [Internet] [Doctoral dissertation]. Texas A&M University; 2016. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/1969.1/158945.

Council of Science Editors:

Johnson KW. Approaches for Modeling Satellite Relative Motion. [Doctoral Dissertation]. Texas A&M University; 2016. Available from: http://hdl.handle.net/1969.1/158945

Penn State University

26. Paik, Ghanghoon. Optimal Orbit Raising Via Particle Swarm Optimization .

Degree: 2015, Penn State University

URL: https://submit-etda.libraries.psu.edu/catalog/25366

► A spacecraft in one orbit may need to move to another orbit. Apoapsis orbit raising, in particular, takes a spacecraft from a circular orbit to…
(more)

Subjects/Keywords: Astrodynamics; Orbit Raising; Particle Swarm Optimization; Trajectory Optimization

Record Details Similar Records

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

APA (6^{th} Edition):

Paik, G. (2015). Optimal Orbit Raising Via Particle Swarm Optimization . (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/25366

Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^{th} Edition):

Paik, Ghanghoon. “Optimal Orbit Raising Via Particle Swarm Optimization .” 2015. Thesis, Penn State University. Accessed March 07, 2021. https://submit-etda.libraries.psu.edu/catalog/25366.

Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^{th} Edition):

Paik, Ghanghoon. “Optimal Orbit Raising Via Particle Swarm Optimization .” 2015. Web. 07 Mar 2021.

Vancouver:

Paik G. Optimal Orbit Raising Via Particle Swarm Optimization . [Internet] [Thesis]. Penn State University; 2015. [cited 2021 Mar 07]. Available from: https://submit-etda.libraries.psu.edu/catalog/25366.

Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Paik G. Optimal Orbit Raising Via Particle Swarm Optimization . [Thesis]. Penn State University; 2015. Available from: https://submit-etda.libraries.psu.edu/catalog/25366

Not specified: Masters Thesis or Doctoral Dissertation

Penn State University

27. Conte, Davide. Semi-Analytical Solutions for Proximity Operations in the Circular Restricted Three-Body Problem.

Degree: 2019, Penn State University

URL: https://submit-etda.libraries.psu.edu/catalog/16596dxc5120

► The research presented in this dissertation aims at characterizing the relative motion between spacecraft in periodic orbits in the circular restricted three-body problem. Proximity operations…
(more)

Subjects/Keywords: Astrodynamics; Moon; Mars; Phobos; Proximity Operations; Relative Motion; Semi-Analytical

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

APA (6^{th} Edition):

Conte, D. (2019). Semi-Analytical Solutions for Proximity Operations in the Circular Restricted Three-Body Problem. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/16596dxc5120

Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^{th} Edition):

Conte, Davide. “Semi-Analytical Solutions for Proximity Operations in the Circular Restricted Three-Body Problem.” 2019. Thesis, Penn State University. Accessed March 07, 2021. https://submit-etda.libraries.psu.edu/catalog/16596dxc5120.

Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^{th} Edition):

Conte, Davide. “Semi-Analytical Solutions for Proximity Operations in the Circular Restricted Three-Body Problem.” 2019. Web. 07 Mar 2021.

Vancouver:

Conte D. Semi-Analytical Solutions for Proximity Operations in the Circular Restricted Three-Body Problem. [Internet] [Thesis]. Penn State University; 2019. [cited 2021 Mar 07]. Available from: https://submit-etda.libraries.psu.edu/catalog/16596dxc5120.

Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Conte D. Semi-Analytical Solutions for Proximity Operations in the Circular Restricted Three-Body Problem. [Thesis]. Penn State University; 2019. Available from: https://submit-etda.libraries.psu.edu/catalog/16596dxc5120

Not specified: Masters Thesis or Doctoral Dissertation

Penn State University

28. Sottile, Brad Joseph. Evolutionary Computation for Spacecraft Trajectory Optimization.

Degree: 2013, Penn State University

URL: https://submit-etda.libraries.psu.edu/catalog/19135

► Evolutionary Computation has exploded in use in engineering and the applied sciences. For this thesis, three algorithms – Particle Swarm Optimization (PSO), Bacteria Foraging Optimization…
(more)

Subjects/Keywords: Astrodynamics; Evolutionary Algorithms; Evolutionary Computation; Evolutionary Strategies; Optimization; Spacecraft Trajectory

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APA (6^{th} Edition):

Sottile, B. J. (2013). Evolutionary Computation for Spacecraft Trajectory Optimization. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/19135

Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^{th} Edition):

Sottile, Brad Joseph. “Evolutionary Computation for Spacecraft Trajectory Optimization.” 2013. Thesis, Penn State University. Accessed March 07, 2021. https://submit-etda.libraries.psu.edu/catalog/19135.

Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^{th} Edition):

Sottile, Brad Joseph. “Evolutionary Computation for Spacecraft Trajectory Optimization.” 2013. Web. 07 Mar 2021.

Vancouver:

Sottile BJ. Evolutionary Computation for Spacecraft Trajectory Optimization. [Internet] [Thesis]. Penn State University; 2013. [cited 2021 Mar 07]. Available from: https://submit-etda.libraries.psu.edu/catalog/19135.

Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Sottile BJ. Evolutionary Computation for Spacecraft Trajectory Optimization. [Thesis]. Penn State University; 2013. Available from: https://submit-etda.libraries.psu.edu/catalog/19135

Not specified: Masters Thesis or Doctoral Dissertation

Penn State University

29. Reiter, Jason A. Numerical And Analytical Solutions To Rapid Collision Avoidance Maneuvers Constrained By Mission Performance Requirements.

Degree: 2016, Penn State University

URL: https://submit-etda.libraries.psu.edu/catalog/29469

► Collision avoidance maneuvers to prevent orbital collisions between two catalogued objects are typically planned multiple days in advance. If the warning time is decreased to…
(more)

Subjects/Keywords: astrodynamics; collision avoidance; debris; trade studies; optimization; trajectory; mission design

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

APA (6^{th} Edition):

Reiter, J. A. (2016). Numerical And Analytical Solutions To Rapid Collision Avoidance Maneuvers Constrained By Mission Performance Requirements. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/29469

Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^{th} Edition):

Reiter, Jason A. “Numerical And Analytical Solutions To Rapid Collision Avoidance Maneuvers Constrained By Mission Performance Requirements.” 2016. Thesis, Penn State University. Accessed March 07, 2021. https://submit-etda.libraries.psu.edu/catalog/29469.

Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^{th} Edition):

Reiter, Jason A. “Numerical And Analytical Solutions To Rapid Collision Avoidance Maneuvers Constrained By Mission Performance Requirements.” 2016. Web. 07 Mar 2021.

Vancouver:

Reiter JA. Numerical And Analytical Solutions To Rapid Collision Avoidance Maneuvers Constrained By Mission Performance Requirements. [Internet] [Thesis]. Penn State University; 2016. [cited 2021 Mar 07]. Available from: https://submit-etda.libraries.psu.edu/catalog/29469.

Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Reiter JA. Numerical And Analytical Solutions To Rapid Collision Avoidance Maneuvers Constrained By Mission Performance Requirements. [Thesis]. Penn State University; 2016. Available from: https://submit-etda.libraries.psu.edu/catalog/29469

Not specified: Masters Thesis or Doctoral Dissertation

Penn State University

30. Kuppa, Koundinya. Long-term Orbit Propagation Using Symplectic Integration Algorithms.

Degree: 2016, Penn State University

URL: https://submit-etda.libraries.psu.edu/catalog/29463

► Understanding the evolution of satellite orbits in the long-term is of great importance in *astrodynamics*. In order to achieve this, accurate propagation of the orbital…
(more)

Subjects/Keywords: astrodynamics; orbital mechanics; symplectic integration; numerical integration; orbit propagation; spaceflight mechanics

Record Details Similar Records

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

APA (6^{th} Edition):

Kuppa, K. (2016). Long-term Orbit Propagation Using Symplectic Integration Algorithms. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/29463

Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^{th} Edition):

Kuppa, Koundinya. “Long-term Orbit Propagation Using Symplectic Integration Algorithms.” 2016. Thesis, Penn State University. Accessed March 07, 2021. https://submit-etda.libraries.psu.edu/catalog/29463.

Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^{th} Edition):

Kuppa, Koundinya. “Long-term Orbit Propagation Using Symplectic Integration Algorithms.” 2016. Web. 07 Mar 2021.

Vancouver:

Kuppa K. Long-term Orbit Propagation Using Symplectic Integration Algorithms. [Internet] [Thesis]. Penn State University; 2016. [cited 2021 Mar 07]. Available from: https://submit-etda.libraries.psu.edu/catalog/29463.

Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Kuppa K. Long-term Orbit Propagation Using Symplectic Integration Algorithms. [Thesis]. Penn State University; 2016. Available from: https://submit-etda.libraries.psu.edu/catalog/29463

Not specified: Masters Thesis or Doctoral Dissertation