Advanced search options

Advanced Search Options 🞨

Browse by author name (“Author name starts with…”).

Find ETDs with:

in
/  
in
/  
in
/  
in

Written in Published in Earliest date Latest date

Sorted by

Results per page:

Sorted by: relevance · author · university · dateNew search

You searched for subject:(Astrodynamics). Showing records 1 – 30 of 137 total matches.

[1] [2] [3] [4] [5]

Search Limiters

Last 2 Years | English Only

Degrees

Levels

Country

▼ Search Limiters


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

  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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th 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 04, 2021. https://commons.erau.edu/edt/251.

MLA Handbook (7th Edition):

Iyengar, Spatika Dasharati. “Computation of Hypersonic Flows with Lateral Jets Using k-ω Turbulence Model.” 2015. Web. 04 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 04]. 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

Astrodynamics and Space Missions

Aerospace Engineering

Advisors/Committee Members: Mooij, E. (mentor), Naeije, M.C. (mentor).

Subjects/Keywords: Astrodynamics

…13 14 16 17 19 20 21 21 22 23 24 4 Astrodynamics and Orbital Mechanics 4.1 Gravity… …of astrodynamics and the space environment with the various perturbations… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th Edition):

Vittaldev, V (author). “The Unified State Model. Derivation and Applications in Astrodynamics and Navigation.” 2010. Masters Thesis, Delft University of Technology. Accessed March 04, 2021. http://resolver.tudelft.nl/uuid:198390b8-b81f-4a13-9c80-15befd3c0428.

MLA Handbook (7th Edition):

Vittaldev, V (author). “The Unified State Model. Derivation and Applications in Astrodynamics and Navigation.” 2010. Web. 04 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 04]. 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

  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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th Edition):

Sestak, Timothy Allen. “The Effect of Surface Materials and Morphology on Wingsuit Aerodynamics.” 2017. Doctoral Dissertation, Embry-Riddle Aeronautical University. Accessed March 04, 2021. https://commons.erau.edu/edt/355.

MLA Handbook (7th Edition):

Sestak, Timothy Allen. “The Effect of Surface Materials and Morphology on Wingsuit Aerodynamics.” 2017. Web. 04 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 04]. 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

 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th Edition):

Kelly, Patrick W. “Orbital Debris Mitigation Using Solar Sail Trajectory Optimization.” 2018. Doctoral Dissertation, University of Florida. Accessed March 04, 2021. https://ufdc.ufl.edu/UFE0053995.

MLA Handbook (7th Edition):

Kelly, Patrick W. “Orbital Debris Mitigation Using Solar Sail Trajectory Optimization.” 2018. Web. 04 Mar 2021.

Vancouver:

Kelly PW. Orbital Debris Mitigation Using Solar Sail Trajectory Optimization. [Internet] [Doctoral dissertation]. University of Florida; 2018. [cited 2021 Mar 04]. 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

 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th Edition):

Farahmand, Mitra. “ORBITAL PROPAGATORS FOR HORIZON SIMULATION FRAMEWORK.” 2009. Masters Thesis, Cal Poly. Accessed March 04, 2021. https://digitalcommons.calpoly.edu/theses/167 ; 10.15368/theses.2009.138.

MLA Handbook (7th Edition):

Farahmand, Mitra. “ORBITAL PROPAGATORS FOR HORIZON SIMULATION FRAMEWORK.” 2009. Web. 04 Mar 2021.

Vancouver:

Farahmand M. ORBITAL PROPAGATORS FOR HORIZON SIMULATION FRAMEWORK. [Internet] [Masters thesis]. Cal Poly; 2009. [cited 2021 Mar 04]. 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

  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 DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th 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 04, 2021. https://docs.lib.purdue.edu/open_access_dissertations/278.

MLA Handbook (7th Edition):

Haapala, Amanda F. “Trajectory design in the spatial circular restricted three-body problem exploiting higher-dimensional Poincare maps.” 2014. Web. 04 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 04]. 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

 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th Edition):

Conte, Davide. “Determination of Optimal Earth-mars Trajectories to Target the Moons of Mars.” 2014. Thesis, Penn State University. Accessed March 04, 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 (7th Edition):

Conte, Davide. “Determination of Optimal Earth-mars Trajectories to Target the Moons of Mars.” 2014. Web. 04 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 04]. 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

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

  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 DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th 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 04, 2021. https://commons.erau.edu/edt/424.

MLA Handbook (7th Edition):

Coulter, Nolan. “Design of an Attitude Control System for a Spacecraft with Propellant Slosh Dynamics.” 2018. Web. 04 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 04]. 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

 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 DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th Edition):

Agrawal, Abhishek (author). “Orbital motion of regolith around asteroids.” 2018. Masters Thesis, Delft University of Technology. Accessed March 04, 2021. http://resolver.tudelft.nl/uuid:0933c1e6-89ee-476c-9b45-3e6d235ddac6.

MLA Handbook (7th Edition):

Agrawal, Abhishek (author). “Orbital motion of regolith around asteroids.” 2018. Web. 04 Mar 2021.

Vancouver:

Agrawal A(. Orbital motion of regolith around asteroids. [Internet] [Masters thesis]. Delft University of Technology; 2018. [cited 2021 Mar 04]. 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

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 DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th 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 04, 2021. http://resolver.tudelft.nl/uuid:1c58ca05-b367-48e6-9b4c-e31f12f488d7.

MLA Handbook (7th Edition):

de Jong, Hanneke (author). “Analytical Low-Thrust Trajectory Design: Using the Simplified General Perturbations Model.” 2018. Web. 04 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 04]. 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

 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 DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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

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):

Ponnapalli, Kaushik. “Optimal variable-specific-impulse trajectories in simple gravitational fields.” 2019. Thesis, University of Illinois – Urbana-Champaign. Accessed March 04, 2021. http://hdl.handle.net/2142/104920.

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

MLA Handbook (7th Edition):

Ponnapalli, Kaushik. “Optimal variable-specific-impulse trajectories in simple gravitational fields.” 2019. Web. 04 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 04]. Available from: http://hdl.handle.net/2142/104920.

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

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

 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 DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th Edition):

Crowe, William. “Use of Spacecraft Swarms to Characterise Asteroids during Flyby.” 2018. Doctoral Dissertation, University of New South Wales. Accessed March 04, 2021. http://handle.unsw.edu.au/1959.4/60892.

MLA Handbook (7th Edition):

Crowe, William. “Use of Spacecraft Swarms to Characterise Asteroids during Flyby.” 2018. Web. 04 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 04]. 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

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 DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th Edition):

Vandenberghe, Alexander (author). “Station-keeping in the vicinity of the collinear Lagrange points.” 2020. Masters Thesis, Delft University of Technology. Accessed March 04, 2021. http://resolver.tudelft.nl/uuid:8b82e473-2ed1-48c4-ac3e-a59ee1a5039c.

MLA Handbook (7th Edition):

Vandenberghe, Alexander (author). “Station-keeping in the vicinity of the collinear Lagrange points.” 2020. Web. 04 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 04]. 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

  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 DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th Edition):

Graef, Jared. “B-Plane Targeting with the Spacecraft Trajectory Optimization Suite.” 2020. Masters Thesis, Cal Poly. Accessed March 04, 2021. https://digitalcommons.calpoly.edu/theses/2251.

MLA Handbook (7th Edition):

Graef, Jared. “B-Plane Targeting with the Spacecraft Trajectory Optimization Suite.” 2020. Web. 04 Mar 2021.

Vancouver:

Graef J. B-Plane Targeting with the Spacecraft Trajectory Optimization Suite. [Internet] [Masters thesis]. Cal Poly; 2020. [cited 2021 Mar 04]. 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

  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 DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Geeraert, Jeroen L. “Multi-Satellite Orbit Determination Using Interferometric Observables with RF Localization Applications.” 2017. Doctoral Dissertation, University of Colorado. Accessed March 04, 2021. https://scholar.colorado.edu/asen_gradetds/192.

MLA Handbook (7th Edition):

Geeraert, Jeroen L. “Multi-Satellite Orbit Determination Using Interferometric Observables with RF Localization Applications.” 2017. Web. 04 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 04]. 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

 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 DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th 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 04, 2021. http://resolver.tudelft.nl/uuid:d9768a7f-0c57-4437-befb-4ccf7a39a0a5.

MLA Handbook (7th Edition):

Villegas Pinto, Daniel (author). “Temporary Capture of Asteroid Ejecta into Periodic Orbits: Application to JAXA’s Hayabusa2 Impact Event.” 2019. Web. 04 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 04]. 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

 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 DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th Edition):

Hess, J R (author). “Aerogravity assists: Hypersonic maneuvering to improve planetary gravity assists.” 2016. Masters Thesis, Delft University of Technology. Accessed March 04, 2021. http://resolver.tudelft.nl/uuid:dee2d842-ca91-4086-8ef8-771cfee1b0dc.

MLA Handbook (7th Edition):

Hess, J R (author). “Aerogravity assists: Hypersonic maneuvering to improve planetary gravity assists.” 2016. Web. 04 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 04]. 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

  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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th Edition):

Iuliano, Jay R. “A Solution to the Circular Restricted N Body Problem in Planetary Systems.” 2016. Masters Thesis, Cal Poly. Accessed March 04, 2021. https://digitalcommons.calpoly.edu/theses/1612 ; 10.15368/theses.2016.80.

MLA Handbook (7th Edition):

Iuliano, Jay R. “A Solution to the Circular Restricted N Body Problem in Planetary Systems.” 2016. Web. 04 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 04]. 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

  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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th Edition):

Jackson, Daniel J. “Formulation of an Optimal Search Strategy for Space Debris At GEO.” 2011. Masters Thesis, Cal Poly. Accessed March 04, 2021. https://digitalcommons.calpoly.edu/theses/656 ; 10.15368/theses.2011.202.

MLA Handbook (7th Edition):

Jackson, Daniel J. “Formulation of an Optimal Search Strategy for Space Debris At GEO.” 2011. Web. 04 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 04]. 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

 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th Edition):

Capon, Christopher. “Ionospheric Aerodynamics in Low Earth Orbit.” 2017. Doctoral Dissertation, University of New South Wales. Accessed March 04, 2021. http://handle.unsw.edu.au/1959.4/58652 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:46528/SOURCE01?view=true.

MLA Handbook (7th Edition):

Capon, Christopher. “Ionospheric Aerodynamics in Low Earth Orbit.” 2017. Web. 04 Mar 2021.

Vancouver:

Capon C. Ionospheric Aerodynamics in Low Earth Orbit. [Internet] [Doctoral dissertation]. University of New South Wales; 2017. [cited 2021 Mar 04]. 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

 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th Edition):

Carvalho Barreira Lages Ribeiro, André (author). “Optimal Aeroassisted Maneuvers for Orbital Transfer.” 2019. Masters Thesis, Delft University of Technology. Accessed March 04, 2021. http://resolver.tudelft.nl/uuid:89acba76-65ed-438d-810e-f3a863546398.

MLA Handbook (7th Edition):

Carvalho Barreira Lages Ribeiro, André (author). “Optimal Aeroassisted Maneuvers for Orbital Transfer.” 2019. Web. 04 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 04]. 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

  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 DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

McMahon, Jay Warren. “An Analytical Theory for the Perturbative Effect of Solar Radiation Pressure on Natural and Artificial Satellites.” 2011. Doctoral Dissertation, University of Colorado. Accessed March 04, 2021. https://scholar.colorado.edu/asen_gradetds/26.

MLA Handbook (7th Edition):

McMahon, Jay Warren. “An Analytical Theory for the Perturbative Effect of Solar Radiation Pressure on Natural and Artificial Satellites.” 2011. Web. 04 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 04]. 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

  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 DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th Edition):

Baresi, Nicola. “Spacecraft Formation Flight on Quasi-Periodic Invariant Tori.” 2017. Doctoral Dissertation, University of Colorado. Accessed March 04, 2021. https://scholar.colorado.edu/asen_gradetds/219.

MLA Handbook (7th Edition):

Baresi, Nicola. “Spacecraft Formation Flight on Quasi-Periodic Invariant Tori.” 2017. Web. 04 Mar 2021.

Vancouver:

Baresi N. Spacecraft Formation Flight on Quasi-Periodic Invariant Tori. [Internet] [Doctoral dissertation]. University of Colorado; 2017. [cited 2021 Mar 04]. 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

  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 DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th 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 04, 2021. https://scholar.colorado.edu/asen_gradetds/235.

MLA Handbook (7th Edition):

De Smet, Stijn. “On the Design of Solar Gravity Driven Planetocentric Transfers Using Artificial Neural Networks.” 2018. Web. 04 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 04]. 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

 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 DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th Edition):

Johnson, Kirk Wayne. “Approaches for Modeling Satellite Relative Motion.” 2016. Doctoral Dissertation, Texas A&M University. Accessed March 04, 2021. http://hdl.handle.net/1969.1/158945.

MLA Handbook (7th Edition):

Johnson, Kirk Wayne. “Approaches for Modeling Satellite Relative Motion.” 2016. Web. 04 Mar 2021.

Vancouver:

Johnson KW. Approaches for Modeling Satellite Relative Motion. [Internet] [Doctoral dissertation]. Texas A&M University; 2016. [cited 2021 Mar 04]. 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

 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 DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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

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):

Paik, Ghanghoon. “Optimal Orbit Raising Via Particle Swarm Optimization .” 2015. Thesis, Penn State University. Accessed March 04, 2021. https://submit-etda.libraries.psu.edu/catalog/25366.

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

MLA Handbook (7th Edition):

Paik, Ghanghoon. “Optimal Orbit Raising Via Particle Swarm Optimization .” 2015. Web. 04 Mar 2021.

Vancouver:

Paik G. Optimal Orbit Raising Via Particle Swarm Optimization . [Internet] [Thesis]. Penn State University; 2015. [cited 2021 Mar 04]. Available from: https://submit-etda.libraries.psu.edu/catalog/25366.

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

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

 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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

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):

Conte, Davide. “Semi-Analytical Solutions for Proximity Operations in the Circular Restricted Three-Body Problem.” 2019. Thesis, Penn State University. Accessed March 04, 2021. https://submit-etda.libraries.psu.edu/catalog/16596dxc5120.

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

MLA Handbook (7th Edition):

Conte, Davide. “Semi-Analytical Solutions for Proximity Operations in the Circular Restricted Three-Body Problem.” 2019. Web. 04 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 04]. Available from: https://submit-etda.libraries.psu.edu/catalog/16596dxc5120.

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. 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

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

 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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

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):

Sottile, Brad Joseph. “Evolutionary Computation for Spacecraft Trajectory Optimization.” 2013. Thesis, Penn State University. Accessed March 04, 2021. https://submit-etda.libraries.psu.edu/catalog/19135.

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

MLA Handbook (7th Edition):

Sottile, Brad Joseph. “Evolutionary Computation for Spacecraft Trajectory Optimization.” 2013. Web. 04 Mar 2021.

Vancouver:

Sottile BJ. Evolutionary Computation for Spacecraft Trajectory Optimization. [Internet] [Thesis]. Penn State University; 2013. [cited 2021 Mar 04]. Available from: https://submit-etda.libraries.psu.edu/catalog/19135.

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

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

 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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

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):

Reiter, Jason A. “Numerical And Analytical Solutions To Rapid Collision Avoidance Maneuvers Constrained By Mission Performance Requirements.” 2016. Thesis, Penn State University. Accessed March 04, 2021. https://submit-etda.libraries.psu.edu/catalog/29469.

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

MLA Handbook (7th Edition):

Reiter, Jason A. “Numerical And Analytical Solutions To Rapid Collision Avoidance Maneuvers Constrained By Mission Performance Requirements.” 2016. Web. 04 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 04]. Available from: https://submit-etda.libraries.psu.edu/catalog/29469.

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

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

 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 DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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

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):

Kuppa, Koundinya. “Long-term Orbit Propagation Using Symplectic Integration Algorithms.” 2016. Thesis, Penn State University. Accessed March 04, 2021. https://submit-etda.libraries.psu.edu/catalog/29463.

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

MLA Handbook (7th Edition):

Kuppa, Koundinya. “Long-term Orbit Propagation Using Symplectic Integration Algorithms.” 2016. Web. 04 Mar 2021.

Vancouver:

Kuppa K. Long-term Orbit Propagation Using Symplectic Integration Algorithms. [Internet] [Thesis]. Penn State University; 2016. [cited 2021 Mar 04]. Available from: https://submit-etda.libraries.psu.edu/catalog/29463.

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

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

[1] [2] [3] [4] [5]

.