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You searched for subject:(Rendezvous). Showing records 1 – 30 of 74 total matches.

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Virginia Tech

1. Karlgaard, Christopher David. Robust Adaptive Estimation for Autonomous Rendezvous in Elliptical Orbit.

Degree: PhD, Aerospace and Ocean Engineering, 2010, Virginia Tech

 The development of navigation filters that make use of robust estimation techniques is important due to the sensitivity of the typical minimum L2 norm techniques,… (more)

Subjects/Keywords: Robust Estimation; Rendezvous; Adaptive Estimation

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APA (6th Edition):

Karlgaard, C. D. (2010). Robust Adaptive Estimation for Autonomous Rendezvous in Elliptical Orbit. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/28274

Chicago Manual of Style (16th Edition):

Karlgaard, Christopher David. “Robust Adaptive Estimation for Autonomous Rendezvous in Elliptical Orbit.” 2010. Doctoral Dissertation, Virginia Tech. Accessed September 27, 2020. http://hdl.handle.net/10919/28274.

MLA Handbook (7th Edition):

Karlgaard, Christopher David. “Robust Adaptive Estimation for Autonomous Rendezvous in Elliptical Orbit.” 2010. Web. 27 Sep 2020.

Vancouver:

Karlgaard CD. Robust Adaptive Estimation for Autonomous Rendezvous in Elliptical Orbit. [Internet] [Doctoral dissertation]. Virginia Tech; 2010. [cited 2020 Sep 27]. Available from: http://hdl.handle.net/10919/28274.

Council of Science Editors:

Karlgaard CD. Robust Adaptive Estimation for Autonomous Rendezvous in Elliptical Orbit. [Doctoral Dissertation]. Virginia Tech; 2010. Available from: http://hdl.handle.net/10919/28274


Luleå University of Technology

2. Regoli, Leonardo. Advanced Attitude Determination using Photonic Mixer Devices.

Degree: 2012, Luleå University of Technology

Photonic Mixer Devices (PMD) have arose as a new and promising technology in imaging devices, providing 3D images at high frame rates by performing… (more)

Subjects/Keywords: Technology; PMD; rendezvous; docking; Teknik

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APA (6th Edition):

Regoli, L. (2012). Advanced Attitude Determination using Photonic Mixer Devices. (Thesis). Luleå University of Technology. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-42803

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):

Regoli, Leonardo. “Advanced Attitude Determination using Photonic Mixer Devices.” 2012. Thesis, Luleå University of Technology. Accessed September 27, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-42803.

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

MLA Handbook (7th Edition):

Regoli, Leonardo. “Advanced Attitude Determination using Photonic Mixer Devices.” 2012. Web. 27 Sep 2020.

Vancouver:

Regoli L. Advanced Attitude Determination using Photonic Mixer Devices. [Internet] [Thesis]. Luleå University of Technology; 2012. [cited 2020 Sep 27]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-42803.

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

Council of Science Editors:

Regoli L. Advanced Attitude Determination using Photonic Mixer Devices. [Thesis]. Luleå University of Technology; 2012. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-42803

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

3. Ghafoor, Saim. Cognitive radio adaptive rendezvous protocols to establish network services for a disaster response.

Degree: 2018, University College Cork

 Disasters are catastrophic events that cause great damage or loss of life. In disasters, communication services might be disrupted due to damage to the existing… (more)

Subjects/Keywords: Blind rendezvous; Fully blind rendezvous; Cognitive radio networks; Disaster response networks; USRP; Prototype for disasters; Multihop rendezvous protocol

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APA (6th Edition):

Ghafoor, S. (2018). Cognitive radio adaptive rendezvous protocols to establish network services for a disaster response. (Thesis). University College Cork. Retrieved from http://hdl.handle.net/10468/7131

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):

Ghafoor, Saim. “Cognitive radio adaptive rendezvous protocols to establish network services for a disaster response.” 2018. Thesis, University College Cork. Accessed September 27, 2020. http://hdl.handle.net/10468/7131.

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

MLA Handbook (7th Edition):

Ghafoor, Saim. “Cognitive radio adaptive rendezvous protocols to establish network services for a disaster response.” 2018. Web. 27 Sep 2020.

Vancouver:

Ghafoor S. Cognitive radio adaptive rendezvous protocols to establish network services for a disaster response. [Internet] [Thesis]. University College Cork; 2018. [cited 2020 Sep 27]. Available from: http://hdl.handle.net/10468/7131.

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

Council of Science Editors:

Ghafoor S. Cognitive radio adaptive rendezvous protocols to establish network services for a disaster response. [Thesis]. University College Cork; 2018. Available from: http://hdl.handle.net/10468/7131

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

4. Fear, Andrew John. CubeSat autonomous rendezvous and docking software.

Degree: MSin Engineering, Aerospace Engineering, 2014, University of Texas – Austin

 An autonomous mission manager is being developed for use on CubeSats to perform proximity operations with other vehicles. The mission manager software is designed to… (more)

Subjects/Keywords: CubeSat; Rendezvous

…Technology Roadmap (TA04 and TA05) [3]. The CubeSat Autonomous Rendezvous and… …distance to 1 m of the desired rendezvous vehicle, known as the target. However, the goal of this… …algorithms have been selected and implemented for autonomous rendezvous operations. 1 The CARDS… …environmental simulation is an analytical setting to test the mission manager software. A rendezvous… …NASA’s “Autonomous Rendezvous and Docking (AR&D) Warehouse.” [5]… 

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APA (6th Edition):

Fear, A. J. (2014). CubeSat autonomous rendezvous and docking software. (Masters Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/28249

Chicago Manual of Style (16th Edition):

Fear, Andrew John. “CubeSat autonomous rendezvous and docking software.” 2014. Masters Thesis, University of Texas – Austin. Accessed September 27, 2020. http://hdl.handle.net/2152/28249.

MLA Handbook (7th Edition):

Fear, Andrew John. “CubeSat autonomous rendezvous and docking software.” 2014. Web. 27 Sep 2020.

Vancouver:

Fear AJ. CubeSat autonomous rendezvous and docking software. [Internet] [Masters thesis]. University of Texas – Austin; 2014. [cited 2020 Sep 27]. Available from: http://hdl.handle.net/2152/28249.

Council of Science Editors:

Fear AJ. CubeSat autonomous rendezvous and docking software. [Masters Thesis]. University of Texas – Austin; 2014. Available from: http://hdl.handle.net/2152/28249


Delft University of Technology

5. Vromen, S.S. (author). Design of Convex Guidance for the Final Phase of Satellite Rendezvous: Tested using Hardware-in-the-Loop Simulations.

Degree: 2015, Delft University of Technology

Over the past decades the steep increase in the number of space-debris objects have sparked many studies into active space-debris removal. Past collisions have shown… (more)

Subjects/Keywords: Rendezvous; Hardware-In-The-Loop; Guidance; Convex

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APA (6th Edition):

Vromen, S. S. (. (2015). Design of Convex Guidance for the Final Phase of Satellite Rendezvous: Tested using Hardware-in-the-Loop Simulations. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:5dc275ca-cdfb-4104-bec8-2d1665cd04a5

Chicago Manual of Style (16th Edition):

Vromen, S S (author). “Design of Convex Guidance for the Final Phase of Satellite Rendezvous: Tested using Hardware-in-the-Loop Simulations.” 2015. Masters Thesis, Delft University of Technology. Accessed September 27, 2020. http://resolver.tudelft.nl/uuid:5dc275ca-cdfb-4104-bec8-2d1665cd04a5.

MLA Handbook (7th Edition):

Vromen, S S (author). “Design of Convex Guidance for the Final Phase of Satellite Rendezvous: Tested using Hardware-in-the-Loop Simulations.” 2015. Web. 27 Sep 2020.

Vancouver:

Vromen SS(. Design of Convex Guidance for the Final Phase of Satellite Rendezvous: Tested using Hardware-in-the-Loop Simulations. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2020 Sep 27]. Available from: http://resolver.tudelft.nl/uuid:5dc275ca-cdfb-4104-bec8-2d1665cd04a5.

Council of Science Editors:

Vromen SS(. Design of Convex Guidance for the Final Phase of Satellite Rendezvous: Tested using Hardware-in-the-Loop Simulations. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:5dc275ca-cdfb-4104-bec8-2d1665cd04a5


University of Illinois – Urbana-Champaign

6. Chan, Nicole. Design and verification of a safe autonomous satellite rendezvous maneuver.

Degree: MS, Electrical & Computer Engr, 2018, University of Illinois – Urbana-Champaign

 A fundamental maneuver in autonomous space operations is known as rendezvous, where an active spacecraft navigates towards and maneuvers within close proximity of a free-flying… (more)

Subjects/Keywords: control; verification; hybrid systems; rendezvous; satellite

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APA (6th Edition):

Chan, N. (2018). Design and verification of a safe autonomous satellite rendezvous maneuver. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/101051

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):

Chan, Nicole. “Design and verification of a safe autonomous satellite rendezvous maneuver.” 2018. Thesis, University of Illinois – Urbana-Champaign. Accessed September 27, 2020. http://hdl.handle.net/2142/101051.

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

MLA Handbook (7th Edition):

Chan, Nicole. “Design and verification of a safe autonomous satellite rendezvous maneuver.” 2018. Web. 27 Sep 2020.

Vancouver:

Chan N. Design and verification of a safe autonomous satellite rendezvous maneuver. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2018. [cited 2020 Sep 27]. Available from: http://hdl.handle.net/2142/101051.

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

Council of Science Editors:

Chan N. Design and verification of a safe autonomous satellite rendezvous maneuver. [Thesis]. University of Illinois – Urbana-Champaign; 2018. Available from: http://hdl.handle.net/2142/101051

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


University of Waterloo

7. Ma, Yan. Coordinated Landing and Mapping with Aerial and Ground Vehicle Teams.

Degree: 2012, University of Waterloo

 Micro Umanned Aerial Vehicle~(UAV) and Umanned Ground Vehicle~(UGV) teams present tremendous opportunities in expanding the range of operations for these vehicles. An effective coordination of… (more)

Subjects/Keywords: Landing; Rendezvous; Quadrotor; UGV; Kinect; SLAM

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APA (6th Edition):

Ma, Y. (2012). Coordinated Landing and Mapping with Aerial and Ground Vehicle Teams. (Thesis). University of Waterloo. Retrieved from http://hdl.handle.net/10012/6993

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

Chicago Manual of Style (16th Edition):

Ma, Yan. “Coordinated Landing and Mapping with Aerial and Ground Vehicle Teams.” 2012. Thesis, University of Waterloo. Accessed September 27, 2020. http://hdl.handle.net/10012/6993.

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

MLA Handbook (7th Edition):

Ma, Yan. “Coordinated Landing and Mapping with Aerial and Ground Vehicle Teams.” 2012. Web. 27 Sep 2020.

Vancouver:

Ma Y. Coordinated Landing and Mapping with Aerial and Ground Vehicle Teams. [Internet] [Thesis]. University of Waterloo; 2012. [cited 2020 Sep 27]. Available from: http://hdl.handle.net/10012/6993.

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

Council of Science Editors:

Ma Y. Coordinated Landing and Mapping with Aerial and Ground Vehicle Teams. [Thesis]. University of Waterloo; 2012. Available from: http://hdl.handle.net/10012/6993

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

8. Li, Peng. Dynamics and Control of Spacecraft Rendezvous By Nonlinear Model Predictive Control.

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

 This doctoral research investigates the fundamental problems in the dynamics and control of spacecraft rendezvous with a non-cooperative tumbling target. New control schemes based on… (more)

Subjects/Keywords: Aerospace engineering; Spacecraft Rendezvous; Proximity Operation; Autonomous Rendezvous; Nonlinear Model Predictive Control

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APA (6th Edition):

Li, P. (2019). Dynamics and Control of Spacecraft Rendezvous By Nonlinear Model Predictive Control. (Doctoral Dissertation). York University. Retrieved from http://hdl.handle.net/10315/35890

Chicago Manual of Style (16th Edition):

Li, Peng. “Dynamics and Control of Spacecraft Rendezvous By Nonlinear Model Predictive Control.” 2019. Doctoral Dissertation, York University. Accessed September 27, 2020. http://hdl.handle.net/10315/35890.

MLA Handbook (7th Edition):

Li, Peng. “Dynamics and Control of Spacecraft Rendezvous By Nonlinear Model Predictive Control.” 2019. Web. 27 Sep 2020.

Vancouver:

Li P. Dynamics and Control of Spacecraft Rendezvous By Nonlinear Model Predictive Control. [Internet] [Doctoral dissertation]. York University; 2019. [cited 2020 Sep 27]. Available from: http://hdl.handle.net/10315/35890.

Council of Science Editors:

Li P. Dynamics and Control of Spacecraft Rendezvous By Nonlinear Model Predictive Control. [Doctoral Dissertation]. York University; 2019. Available from: http://hdl.handle.net/10315/35890

9. 양, 민재. Usefulness of combined percutaneous-endoscopic rendezvous techniques after failed therapeutic endoscopic retrograde cholangiography in the era of endoscopic ultrasound guided rendezvous.

Degree: 2018, Ajou University

The rendezvous approach is a salvage technique after failure of endoscopic retrograde cholangiography (ERC). In certain circumstances, percutaneous-endoscopic rendezvous (PE-RV) is preferred, and endoscopic ultrasound-guided… (more)

Subjects/Keywords: Endoscopic retrograde cholangiopancreatography; Percutaneous endoscopic rendezvous; Endoscopic ultrasound guided rendezvous; 역행성췌담도내시경; 경피-내시경적 랑데부; 내시경초음파 유도하 랑데부

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APA (6th Edition):

양, . (2018). Usefulness of combined percutaneous-endoscopic rendezvous techniques after failed therapeutic endoscopic retrograde cholangiography in the era of endoscopic ultrasound guided rendezvous. (Thesis). Ajou University. Retrieved from http://repository.ajou.ac.kr/handle/201003/16587 ; http://dcoll.ajou.ac.kr:9080/dcollection/jsp/common/DcLoOrgPer.jsp?sItemId=000000027613

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):

양, 민재. “Usefulness of combined percutaneous-endoscopic rendezvous techniques after failed therapeutic endoscopic retrograde cholangiography in the era of endoscopic ultrasound guided rendezvous.” 2018. Thesis, Ajou University. Accessed September 27, 2020. http://repository.ajou.ac.kr/handle/201003/16587 ; http://dcoll.ajou.ac.kr:9080/dcollection/jsp/common/DcLoOrgPer.jsp?sItemId=000000027613.

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

MLA Handbook (7th Edition):

양, 민재. “Usefulness of combined percutaneous-endoscopic rendezvous techniques after failed therapeutic endoscopic retrograde cholangiography in the era of endoscopic ultrasound guided rendezvous.” 2018. Web. 27 Sep 2020.

Vancouver:

양 . Usefulness of combined percutaneous-endoscopic rendezvous techniques after failed therapeutic endoscopic retrograde cholangiography in the era of endoscopic ultrasound guided rendezvous. [Internet] [Thesis]. Ajou University; 2018. [cited 2020 Sep 27]. Available from: http://repository.ajou.ac.kr/handle/201003/16587 ; http://dcoll.ajou.ac.kr:9080/dcollection/jsp/common/DcLoOrgPer.jsp?sItemId=000000027613.

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

Council of Science Editors:

양 . Usefulness of combined percutaneous-endoscopic rendezvous techniques after failed therapeutic endoscopic retrograde cholangiography in the era of endoscopic ultrasound guided rendezvous. [Thesis]. Ajou University; 2018. Available from: http://repository.ajou.ac.kr/handle/201003/16587 ; http://dcoll.ajou.ac.kr:9080/dcollection/jsp/common/DcLoOrgPer.jsp?sItemId=000000027613

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

10. Okasha, Mohamed Elsayed Aly Abd Elaziz. Dynamics and Control of Satellite Relative Motion in Proximity Operations.

Degree: PhD, Aerospace Engineering, 2012, Old Dominion University

  In this dissertation, the development of relative navigation, guidance, and control algorithms of an autonomous space rendezvous and docking system are presented. These algorithms… (more)

Subjects/Keywords: Orbit rendezvous; Proximity operations; Relative motion; Relative nevigation; Satellite formation; Space rendezvous; Aerospace Engineering; Electrical and Computer Engineering; Mechanical Engineering

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APA (6th Edition):

Okasha, M. E. A. A. E. (2012). Dynamics and Control of Satellite Relative Motion in Proximity Operations. (Doctoral Dissertation). Old Dominion University. Retrieved from 9781267350398 ; https://digitalcommons.odu.edu/mae_etds/150

Chicago Manual of Style (16th Edition):

Okasha, Mohamed Elsayed Aly Abd Elaziz. “Dynamics and Control of Satellite Relative Motion in Proximity Operations.” 2012. Doctoral Dissertation, Old Dominion University. Accessed September 27, 2020. 9781267350398 ; https://digitalcommons.odu.edu/mae_etds/150.

MLA Handbook (7th Edition):

Okasha, Mohamed Elsayed Aly Abd Elaziz. “Dynamics and Control of Satellite Relative Motion in Proximity Operations.” 2012. Web. 27 Sep 2020.

Vancouver:

Okasha MEAAE. Dynamics and Control of Satellite Relative Motion in Proximity Operations. [Internet] [Doctoral dissertation]. Old Dominion University; 2012. [cited 2020 Sep 27]. Available from: 9781267350398 ; https://digitalcommons.odu.edu/mae_etds/150.

Council of Science Editors:

Okasha MEAAE. Dynamics and Control of Satellite Relative Motion in Proximity Operations. [Doctoral Dissertation]. Old Dominion University; 2012. Available from: 9781267350398 ; https://digitalcommons.odu.edu/mae_etds/150


University of Toronto

11. Furtado, Joshua Savio. Multi-UAV Path Planning and Guidance for Cooperative Hunting in a Cluttered Environment.

Degree: 2018, University of Toronto

This thesis presents a path planning and guidance algorithm for cooperative hunting by a group of multi-rotor Unmanned Aerial Vehicles (UAVs). A group of intelligent… (more)

Subjects/Keywords: Collision avoidance; Cooperative hunting; Guidance; Path planning; Rendezvous; UAV; 0538

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APA (6th Edition):

Furtado, J. S. (2018). Multi-UAV Path Planning and Guidance for Cooperative Hunting in a Cluttered Environment. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/98529

Chicago Manual of Style (16th Edition):

Furtado, Joshua Savio. “Multi-UAV Path Planning and Guidance for Cooperative Hunting in a Cluttered Environment.” 2018. Masters Thesis, University of Toronto. Accessed September 27, 2020. http://hdl.handle.net/1807/98529.

MLA Handbook (7th Edition):

Furtado, Joshua Savio. “Multi-UAV Path Planning and Guidance for Cooperative Hunting in a Cluttered Environment.” 2018. Web. 27 Sep 2020.

Vancouver:

Furtado JS. Multi-UAV Path Planning and Guidance for Cooperative Hunting in a Cluttered Environment. [Internet] [Masters thesis]. University of Toronto; 2018. [cited 2020 Sep 27]. Available from: http://hdl.handle.net/1807/98529.

Council of Science Editors:

Furtado JS. Multi-UAV Path Planning and Guidance for Cooperative Hunting in a Cluttered Environment. [Masters Thesis]. University of Toronto; 2018. Available from: http://hdl.handle.net/1807/98529


Delft University of Technology

12. Timmer, M. (author). Rendezvous on an interval and a search game on a star.

Degree: Electrical Engineering, Mathematics, Computer Sci, Applied Mathematics, 2008, Delft University of Technology

Rendezvous problems and search games (with two players) are related problems. In a rendezvous problem the players like to meet as soon as possible, while… (more)

Subjects/Keywords: rendezvous; search game; interval; star

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APA (6th Edition):

Timmer, M. (. (2008). Rendezvous on an interval and a search game on a star. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:9e062646-1f23-48cf-bfc0-90eb58d7ab4a

Chicago Manual of Style (16th Edition):

Timmer, M (author). “Rendezvous on an interval and a search game on a star.” 2008. Masters Thesis, Delft University of Technology. Accessed September 27, 2020. http://resolver.tudelft.nl/uuid:9e062646-1f23-48cf-bfc0-90eb58d7ab4a.

MLA Handbook (7th Edition):

Timmer, M (author). “Rendezvous on an interval and a search game on a star.” 2008. Web. 27 Sep 2020.

Vancouver:

Timmer M(. Rendezvous on an interval and a search game on a star. [Internet] [Masters thesis]. Delft University of Technology; 2008. [cited 2020 Sep 27]. Available from: http://resolver.tudelft.nl/uuid:9e062646-1f23-48cf-bfc0-90eb58d7ab4a.

Council of Science Editors:

Timmer M(. Rendezvous on an interval and a search game on a star. [Masters Thesis]. Delft University of Technology; 2008. Available from: http://resolver.tudelft.nl/uuid:9e062646-1f23-48cf-bfc0-90eb58d7ab4a


University of Arizona

13. Daugherty, William Lester, 1928-. Analysis of relative motion and thrust requirements in the terminal phase of rendezvous .

Degree: 1963, University of Arizona

Subjects/Keywords: Orbital rendezvous (Space flight); Motion.

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APA (6th Edition):

Daugherty, William Lester, 1. (1963). Analysis of relative motion and thrust requirements in the terminal phase of rendezvous . (Masters Thesis). University of Arizona. Retrieved from http://hdl.handle.net/10150/319466

Chicago Manual of Style (16th Edition):

Daugherty, William Lester, 1928-. “Analysis of relative motion and thrust requirements in the terminal phase of rendezvous .” 1963. Masters Thesis, University of Arizona. Accessed September 27, 2020. http://hdl.handle.net/10150/319466.

MLA Handbook (7th Edition):

Daugherty, William Lester, 1928-. “Analysis of relative motion and thrust requirements in the terminal phase of rendezvous .” 1963. Web. 27 Sep 2020.

Vancouver:

Daugherty, William Lester 1. Analysis of relative motion and thrust requirements in the terminal phase of rendezvous . [Internet] [Masters thesis]. University of Arizona; 1963. [cited 2020 Sep 27]. Available from: http://hdl.handle.net/10150/319466.

Council of Science Editors:

Daugherty, William Lester 1. Analysis of relative motion and thrust requirements in the terminal phase of rendezvous . [Masters Thesis]. University of Arizona; 1963. Available from: http://hdl.handle.net/10150/319466


University of Arizona

14. Fraser, Robert Bruce, 1939-. Characteristic velocity requirements for rendezvous between non co-planar orbits .

Degree: 1963, University of Arizona

Subjects/Keywords: Orbital rendezvous (Space flight)

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APA (6th Edition):

Fraser, Robert Bruce, 1. (1963). Characteristic velocity requirements for rendezvous between non co-planar orbits . (Masters Thesis). University of Arizona. Retrieved from http://hdl.handle.net/10150/319512

Chicago Manual of Style (16th Edition):

Fraser, Robert Bruce, 1939-. “Characteristic velocity requirements for rendezvous between non co-planar orbits .” 1963. Masters Thesis, University of Arizona. Accessed September 27, 2020. http://hdl.handle.net/10150/319512.

MLA Handbook (7th Edition):

Fraser, Robert Bruce, 1939-. “Characteristic velocity requirements for rendezvous between non co-planar orbits .” 1963. Web. 27 Sep 2020.

Vancouver:

Fraser, Robert Bruce 1. Characteristic velocity requirements for rendezvous between non co-planar orbits . [Internet] [Masters thesis]. University of Arizona; 1963. [cited 2020 Sep 27]. Available from: http://hdl.handle.net/10150/319512.

Council of Science Editors:

Fraser, Robert Bruce 1. Characteristic velocity requirements for rendezvous between non co-planar orbits . [Masters Thesis]. University of Arizona; 1963. Available from: http://hdl.handle.net/10150/319512


Utah State University

15. Phillips, Michael R. Spacecraft Collision Probability Estimation for Rendezvous and Proximity Operations.

Degree: MS, Mechanical and Aerospace Engineering, 2012, Utah State University

  The topic of this thesis is on-board estimation of spacecraft collision probability for orbital rendezvous and proximity operations. All of the examples shown in… (more)

Subjects/Keywords: collision probability; monte carlo; proximity operations; rendezvous; Aerospace Engineering; Engineering

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APA (6th Edition):

Phillips, M. R. (2012). Spacecraft Collision Probability Estimation for Rendezvous and Proximity Operations. (Masters Thesis). Utah State University. Retrieved from https://digitalcommons.usu.edu/etd/1398

Chicago Manual of Style (16th Edition):

Phillips, Michael R. “Spacecraft Collision Probability Estimation for Rendezvous and Proximity Operations.” 2012. Masters Thesis, Utah State University. Accessed September 27, 2020. https://digitalcommons.usu.edu/etd/1398.

MLA Handbook (7th Edition):

Phillips, Michael R. “Spacecraft Collision Probability Estimation for Rendezvous and Proximity Operations.” 2012. Web. 27 Sep 2020.

Vancouver:

Phillips MR. Spacecraft Collision Probability Estimation for Rendezvous and Proximity Operations. [Internet] [Masters thesis]. Utah State University; 2012. [cited 2020 Sep 27]. Available from: https://digitalcommons.usu.edu/etd/1398.

Council of Science Editors:

Phillips MR. Spacecraft Collision Probability Estimation for Rendezvous and Proximity Operations. [Masters Thesis]. Utah State University; 2012. Available from: https://digitalcommons.usu.edu/etd/1398


Georgia Tech

16. Casey, John Alexander. A methodology for sequential low thrust trajectory optimization using prediction models derived from machine learning techniques.

Degree: MS, Aerospace Engineering, 2019, Georgia Tech

 Spacecraft trajectory sequence optimization has been a well-known problem for many years. Difficulty in finding adequate solutions arises from the combinatorial explosion of possible sequences… (more)

Subjects/Keywords: Spacecraft optimization; Low thrust trajectory optimization; Low thrust spacecraft; Machine learning; Regression; Classification; Gradient boosting; Artificial neural networks; Asteroid rendezvous; GTOC; Travelling salesman problem; Methodology; Asteroid rendezvous

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APA (6th Edition):

Casey, J. A. (2019). A methodology for sequential low thrust trajectory optimization using prediction models derived from machine learning techniques. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/61317

Chicago Manual of Style (16th Edition):

Casey, John Alexander. “A methodology for sequential low thrust trajectory optimization using prediction models derived from machine learning techniques.” 2019. Masters Thesis, Georgia Tech. Accessed September 27, 2020. http://hdl.handle.net/1853/61317.

MLA Handbook (7th Edition):

Casey, John Alexander. “A methodology for sequential low thrust trajectory optimization using prediction models derived from machine learning techniques.” 2019. Web. 27 Sep 2020.

Vancouver:

Casey JA. A methodology for sequential low thrust trajectory optimization using prediction models derived from machine learning techniques. [Internet] [Masters thesis]. Georgia Tech; 2019. [cited 2020 Sep 27]. Available from: http://hdl.handle.net/1853/61317.

Council of Science Editors:

Casey JA. A methodology for sequential low thrust trajectory optimization using prediction models derived from machine learning techniques. [Masters Thesis]. Georgia Tech; 2019. Available from: http://hdl.handle.net/1853/61317


Ohio University

17. Scheithauer, Amy T. 3D Relative Position and Orientation Estimation for Rendezvous and Docking Applications Using a 3D Imager.

Degree: MS, Electrical Engineering (Engineering and Technology), 2010, Ohio University

  This research investigates 4-rotor Uninhabited Aerial Vehicle (UAV) rendezvous and docking precision navigation using 3D imaging sensor data and MATLAB software. The orientation of… (more)

Subjects/Keywords: Electrical Engineering; 3D Imaging; LIDAR; Rendezvous and Docking; 3D Image Processing; Navigation; Attitude Determination

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APA (6th Edition):

Scheithauer, A. T. (2010). 3D Relative Position and Orientation Estimation for Rendezvous and Docking Applications Using a 3D Imager. (Masters Thesis). Ohio University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1265809623

Chicago Manual of Style (16th Edition):

Scheithauer, Amy T. “3D Relative Position and Orientation Estimation for Rendezvous and Docking Applications Using a 3D Imager.” 2010. Masters Thesis, Ohio University. Accessed September 27, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1265809623.

MLA Handbook (7th Edition):

Scheithauer, Amy T. “3D Relative Position and Orientation Estimation for Rendezvous and Docking Applications Using a 3D Imager.” 2010. Web. 27 Sep 2020.

Vancouver:

Scheithauer AT. 3D Relative Position and Orientation Estimation for Rendezvous and Docking Applications Using a 3D Imager. [Internet] [Masters thesis]. Ohio University; 2010. [cited 2020 Sep 27]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1265809623.

Council of Science Editors:

Scheithauer AT. 3D Relative Position and Orientation Estimation for Rendezvous and Docking Applications Using a 3D Imager. [Masters Thesis]. Ohio University; 2010. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1265809623


Michigan Technological University

18. Gou, Li. Guaranteed Rendezvous for Cognitive Radio Networks Based on Cycle Length.

Degree: MS, Department of Computer Science, 2017, Michigan Technological University

Rendezvous is a fundamental process establishing a communication link on common channel between a pair of nodes in the cognitive radio networks. How to… (more)

Subjects/Keywords: Rendezvous; Channel Hopping; Cycle Length; Cognitive Radio Network; Digital Communications and Networking

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APA (6th Edition):

Gou, L. (2017). Guaranteed Rendezvous for Cognitive Radio Networks Based on Cycle Length. (Masters Thesis). Michigan Technological University. Retrieved from http://digitalcommons.mtu.edu/etdr/505

Chicago Manual of Style (16th Edition):

Gou, Li. “Guaranteed Rendezvous for Cognitive Radio Networks Based on Cycle Length.” 2017. Masters Thesis, Michigan Technological University. Accessed September 27, 2020. http://digitalcommons.mtu.edu/etdr/505.

MLA Handbook (7th Edition):

Gou, Li. “Guaranteed Rendezvous for Cognitive Radio Networks Based on Cycle Length.” 2017. Web. 27 Sep 2020.

Vancouver:

Gou L. Guaranteed Rendezvous for Cognitive Radio Networks Based on Cycle Length. [Internet] [Masters thesis]. Michigan Technological University; 2017. [cited 2020 Sep 27]. Available from: http://digitalcommons.mtu.edu/etdr/505.

Council of Science Editors:

Gou L. Guaranteed Rendezvous for Cognitive Radio Networks Based on Cycle Length. [Masters Thesis]. Michigan Technological University; 2017. Available from: http://digitalcommons.mtu.edu/etdr/505


Texas A&M University

19. Stancliffe, Devin Aldin. Analysis and Design of a Test Apparatus for Resolving Near-Field Effects Associated With Using a Coarse Sun Sensor as Part of a 6-DOF Solution.

Degree: MS, Aerospace Engineering, 2011, Texas A&M University

 Though the Aerospace industry is moving towards small satellites and smaller sensor technologies, sensors used for close-proximity operations are generally cost (and often size and… (more)

Subjects/Keywords: Coarse sun sensors; 6-dof; near-field effects; NorthStar; close-proximity; autonomous rendezvous and docking

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APA (6th Edition):

Stancliffe, D. A. (2011). Analysis and Design of a Test Apparatus for Resolving Near-Field Effects Associated With Using a Coarse Sun Sensor as Part of a 6-DOF Solution. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2010-08-8440

Chicago Manual of Style (16th Edition):

Stancliffe, Devin Aldin. “Analysis and Design of a Test Apparatus for Resolving Near-Field Effects Associated With Using a Coarse Sun Sensor as Part of a 6-DOF Solution.” 2011. Masters Thesis, Texas A&M University. Accessed September 27, 2020. http://hdl.handle.net/1969.1/ETD-TAMU-2010-08-8440.

MLA Handbook (7th Edition):

Stancliffe, Devin Aldin. “Analysis and Design of a Test Apparatus for Resolving Near-Field Effects Associated With Using a Coarse Sun Sensor as Part of a 6-DOF Solution.” 2011. Web. 27 Sep 2020.

Vancouver:

Stancliffe DA. Analysis and Design of a Test Apparatus for Resolving Near-Field Effects Associated With Using a Coarse Sun Sensor as Part of a 6-DOF Solution. [Internet] [Masters thesis]. Texas A&M University; 2011. [cited 2020 Sep 27]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-08-8440.

Council of Science Editors:

Stancliffe DA. Analysis and Design of a Test Apparatus for Resolving Near-Field Effects Associated With Using a Coarse Sun Sensor as Part of a 6-DOF Solution. [Masters Thesis]. Texas A&M University; 2011. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-08-8440


Texas A&M University

20. Sengupta, Prasenjit. Dynamics and control of satellite relative motion in a central gravitational field.

Degree: PhD, Aerospace Engineering, 2007, Texas A&M University

 The study of satellite relative motion has been of great historic interest, primarily due to its application to rendezvous, intercept, and docking maneuvers, between spacecraft… (more)

Subjects/Keywords: Relative Motion; Rendezvous; Formation Flight; J2

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APA (6th Edition):

Sengupta, P. (2007). Dynamics and control of satellite relative motion in a central gravitational field. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/4724

Chicago Manual of Style (16th Edition):

Sengupta, Prasenjit. “Dynamics and control of satellite relative motion in a central gravitational field.” 2007. Doctoral Dissertation, Texas A&M University. Accessed September 27, 2020. http://hdl.handle.net/1969.1/4724.

MLA Handbook (7th Edition):

Sengupta, Prasenjit. “Dynamics and control of satellite relative motion in a central gravitational field.” 2007. Web. 27 Sep 2020.

Vancouver:

Sengupta P. Dynamics and control of satellite relative motion in a central gravitational field. [Internet] [Doctoral dissertation]. Texas A&M University; 2007. [cited 2020 Sep 27]. Available from: http://hdl.handle.net/1969.1/4724.

Council of Science Editors:

Sengupta P. Dynamics and control of satellite relative motion in a central gravitational field. [Doctoral Dissertation]. Texas A&M University; 2007. Available from: http://hdl.handle.net/1969.1/4724


Brigham Young University

21. Owen, Mark Andrew. Aerial Rendezvous Between an Unmanned Air Vehicle and an Orbiting Target Vehicle.

Degree: MS, 2011, Brigham Young University

 In this thesis we develop methods that facilitate an aerial rendezvous between two air vehicles. The objective of this research is to produce a method… (more)

Subjects/Keywords: aerial rendezvous; vector field; path following; dubins airplane; time optimal; uav; mav; Mechanical Engineering

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APA (6th Edition):

Owen, M. A. (2011). Aerial Rendezvous Between an Unmanned Air Vehicle and an Orbiting Target Vehicle. (Masters Thesis). Brigham Young University. Retrieved from https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=3880&context=etd

Chicago Manual of Style (16th Edition):

Owen, Mark Andrew. “Aerial Rendezvous Between an Unmanned Air Vehicle and an Orbiting Target Vehicle.” 2011. Masters Thesis, Brigham Young University. Accessed September 27, 2020. https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=3880&context=etd.

MLA Handbook (7th Edition):

Owen, Mark Andrew. “Aerial Rendezvous Between an Unmanned Air Vehicle and an Orbiting Target Vehicle.” 2011. Web. 27 Sep 2020.

Vancouver:

Owen MA. Aerial Rendezvous Between an Unmanned Air Vehicle and an Orbiting Target Vehicle. [Internet] [Masters thesis]. Brigham Young University; 2011. [cited 2020 Sep 27]. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=3880&context=etd.

Council of Science Editors:

Owen MA. Aerial Rendezvous Between an Unmanned Air Vehicle and an Orbiting Target Vehicle. [Masters Thesis]. Brigham Young University; 2011. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=3880&context=etd


Luleå University of Technology

22. Ilyas, Daood. Orbital Propagation and Formation Flying of CubeSats within QB50 Constellation.

Degree: 2011, Luleå University of Technology

QB50 project is an initiative of Von Karman Institute, Belgium, which will use an international network of 50 CubeSats for multi-point, in-situ measurements in… (more)

Subjects/Keywords: Technology; orbital propagation; formation flying; QB50 constellation; clohessy wiltshire equations; satellite rendezvous; Teknik

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APA (6th Edition):

Ilyas, D. (2011). Orbital Propagation and Formation Flying of CubeSats within QB50 Constellation. (Thesis). Luleå University of Technology. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-57589

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):

Ilyas, Daood. “Orbital Propagation and Formation Flying of CubeSats within QB50 Constellation.” 2011. Thesis, Luleå University of Technology. Accessed September 27, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-57589.

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

MLA Handbook (7th Edition):

Ilyas, Daood. “Orbital Propagation and Formation Flying of CubeSats within QB50 Constellation.” 2011. Web. 27 Sep 2020.

Vancouver:

Ilyas D. Orbital Propagation and Formation Flying of CubeSats within QB50 Constellation. [Internet] [Thesis]. Luleå University of Technology; 2011. [cited 2020 Sep 27]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-57589.

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

Council of Science Editors:

Ilyas D. Orbital Propagation and Formation Flying of CubeSats within QB50 Constellation. [Thesis]. Luleå University of Technology; 2011. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-57589

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


Michigan State University

23. Harrison, Eugene. Minimum energy space rendezvous.

Degree: PhD, 1962, Michigan State University

Subjects/Keywords: Orbital rendezvous (Space flight); Space flight

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APA (6th Edition):

Harrison, E. (1962). Minimum energy space rendezvous. (Doctoral Dissertation). Michigan State University. Retrieved from http://etd.lib.msu.edu/islandora/object/etd:18547

Chicago Manual of Style (16th Edition):

Harrison, Eugene. “Minimum energy space rendezvous.” 1962. Doctoral Dissertation, Michigan State University. Accessed September 27, 2020. http://etd.lib.msu.edu/islandora/object/etd:18547.

MLA Handbook (7th Edition):

Harrison, Eugene. “Minimum energy space rendezvous.” 1962. Web. 27 Sep 2020.

Vancouver:

Harrison E. Minimum energy space rendezvous. [Internet] [Doctoral dissertation]. Michigan State University; 1962. [cited 2020 Sep 27]. Available from: http://etd.lib.msu.edu/islandora/object/etd:18547.

Council of Science Editors:

Harrison E. Minimum energy space rendezvous. [Doctoral Dissertation]. Michigan State University; 1962. Available from: http://etd.lib.msu.edu/islandora/object/etd:18547


Rice University

24. Mand, Kuljit. Rendezvous and Proximity Operations at the Earth-Moon L2 Lagrange Point: Navigation Analysis for Preliminary Trajectory Design.

Degree: MS, Engineering, 2014, Rice University

 The Earth-Moon L2 point has attracted attention for potential space exploration, and rendezvous is required for several critical operations. The relative dynamics at this location… (more)

Subjects/Keywords: automated sensor determination; LinCov; L2; rendezvous; targeting algorithms; proximity operations; navigation analysis

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APA (6th Edition):

Mand, K. (2014). Rendezvous and Proximity Operations at the Earth-Moon L2 Lagrange Point: Navigation Analysis for Preliminary Trajectory Design. (Masters Thesis). Rice University. Retrieved from http://hdl.handle.net/1911/88095

Chicago Manual of Style (16th Edition):

Mand, Kuljit. “Rendezvous and Proximity Operations at the Earth-Moon L2 Lagrange Point: Navigation Analysis for Preliminary Trajectory Design.” 2014. Masters Thesis, Rice University. Accessed September 27, 2020. http://hdl.handle.net/1911/88095.

MLA Handbook (7th Edition):

Mand, Kuljit. “Rendezvous and Proximity Operations at the Earth-Moon L2 Lagrange Point: Navigation Analysis for Preliminary Trajectory Design.” 2014. Web. 27 Sep 2020.

Vancouver:

Mand K. Rendezvous and Proximity Operations at the Earth-Moon L2 Lagrange Point: Navigation Analysis for Preliminary Trajectory Design. [Internet] [Masters thesis]. Rice University; 2014. [cited 2020 Sep 27]. Available from: http://hdl.handle.net/1911/88095.

Council of Science Editors:

Mand K. Rendezvous and Proximity Operations at the Earth-Moon L2 Lagrange Point: Navigation Analysis for Preliminary Trajectory Design. [Masters Thesis]. Rice University; 2014. Available from: http://hdl.handle.net/1911/88095


Texas A&M University

25. Hart, Jeremy Jay. Methodology for prototyping increased levels of automation for spacecraft rendezvous functions.

Degree: MS, Aerospace Engineering, 2009, Texas A&M University

 The Crew Exploration Vehicle (CEV) necessitates higher levels of automation than previous NASA vehicles due to program requirements for automation, including Automated Rendezvous and Docking… (more)

Subjects/Keywords: Automation; Spacecraft; Rendezvous; Decision-making; Fuzzy Logic

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APA (6th Edition):

Hart, J. J. (2009). Methodology for prototyping increased levels of automation for spacecraft rendezvous functions. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1220

Chicago Manual of Style (16th Edition):

Hart, Jeremy Jay. “Methodology for prototyping increased levels of automation for spacecraft rendezvous functions.” 2009. Masters Thesis, Texas A&M University. Accessed September 27, 2020. http://hdl.handle.net/1969.1/ETD-TAMU-1220.

MLA Handbook (7th Edition):

Hart, Jeremy Jay. “Methodology for prototyping increased levels of automation for spacecraft rendezvous functions.” 2009. Web. 27 Sep 2020.

Vancouver:

Hart JJ. Methodology for prototyping increased levels of automation for spacecraft rendezvous functions. [Internet] [Masters thesis]. Texas A&M University; 2009. [cited 2020 Sep 27]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1220.

Council of Science Editors:

Hart JJ. Methodology for prototyping increased levels of automation for spacecraft rendezvous functions. [Masters Thesis]. Texas A&M University; 2009. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1220


Texas A&M University

26. Aures-Cavalieri, Kurt D. Incomplete Information Pursuit-Evasion Games with Applications to Spacecraft Rendezvous and Missile Defense.

Degree: PhD, Aerospace Engineering, 2014, Texas A&M University

 Pursuit-evasion games reside at the intersection of game theory and optimal control theory. They are often referred to as differential games because the dynamics of… (more)

Subjects/Keywords: differential games; pursuit-evasion, game theory; estimation; optimal control; dynamic inversion; behavior learning; spacecraft rendezvous; missile defense; missile interception

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APA (6th Edition):

Aures-Cavalieri, K. D. (2014). Incomplete Information Pursuit-Evasion Games with Applications to Spacecraft Rendezvous and Missile Defense. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/154101

Chicago Manual of Style (16th Edition):

Aures-Cavalieri, Kurt D. “Incomplete Information Pursuit-Evasion Games with Applications to Spacecraft Rendezvous and Missile Defense.” 2014. Doctoral Dissertation, Texas A&M University. Accessed September 27, 2020. http://hdl.handle.net/1969.1/154101.

MLA Handbook (7th Edition):

Aures-Cavalieri, Kurt D. “Incomplete Information Pursuit-Evasion Games with Applications to Spacecraft Rendezvous and Missile Defense.” 2014. Web. 27 Sep 2020.

Vancouver:

Aures-Cavalieri KD. Incomplete Information Pursuit-Evasion Games with Applications to Spacecraft Rendezvous and Missile Defense. [Internet] [Doctoral dissertation]. Texas A&M University; 2014. [cited 2020 Sep 27]. Available from: http://hdl.handle.net/1969.1/154101.

Council of Science Editors:

Aures-Cavalieri KD. Incomplete Information Pursuit-Evasion Games with Applications to Spacecraft Rendezvous and Missile Defense. [Doctoral Dissertation]. Texas A&M University; 2014. Available from: http://hdl.handle.net/1969.1/154101


Virginia Tech

27. Bian, Kaigui. Medium Access Control in Cognitive Radio Networks.

Degree: PhD, Electrical and Computer Engineering, 2011, Virginia Tech

 Cognitive radio (CR) is seen as one of the enabling technologies for realizing a new regulatory spectrum management paradigm, viz. opportunistic spectrum sharing (OSS). In… (more)

Subjects/Keywords: cognitive radio; coexistence; medium access control; control channel; rendezvous; channel hopping; channel assignment; opportunistic spectrum sharing; dynamic spectrum access

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APA (6th Edition):

Bian, K. (2011). Medium Access Control in Cognitive Radio Networks. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/37591

Chicago Manual of Style (16th Edition):

Bian, Kaigui. “Medium Access Control in Cognitive Radio Networks.” 2011. Doctoral Dissertation, Virginia Tech. Accessed September 27, 2020. http://hdl.handle.net/10919/37591.

MLA Handbook (7th Edition):

Bian, Kaigui. “Medium Access Control in Cognitive Radio Networks.” 2011. Web. 27 Sep 2020.

Vancouver:

Bian K. Medium Access Control in Cognitive Radio Networks. [Internet] [Doctoral dissertation]. Virginia Tech; 2011. [cited 2020 Sep 27]. Available from: http://hdl.handle.net/10919/37591.

Council of Science Editors:

Bian K. Medium Access Control in Cognitive Radio Networks. [Doctoral Dissertation]. Virginia Tech; 2011. Available from: http://hdl.handle.net/10919/37591


Virginia Tech

28. Kruep, John M. Six degree of freedom optimal trajectories for satellite rendezvous.

Degree: MS, Aerospace Engineering, 1996, Virginia Tech

  A method is developed for computing the minimum fuel trajectory for a satellite that moves between two different positions and orientations using a sequence… (more)

Subjects/Keywords: optimization; trajectory; rendezvous; satellites; LD5655.V855 1996.K784

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APA (6th Edition):

Kruep, J. M. (1996). Six degree of freedom optimal trajectories for satellite rendezvous. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/41037

Chicago Manual of Style (16th Edition):

Kruep, John M. “Six degree of freedom optimal trajectories for satellite rendezvous.” 1996. Masters Thesis, Virginia Tech. Accessed September 27, 2020. http://hdl.handle.net/10919/41037.

MLA Handbook (7th Edition):

Kruep, John M. “Six degree of freedom optimal trajectories for satellite rendezvous.” 1996. Web. 27 Sep 2020.

Vancouver:

Kruep JM. Six degree of freedom optimal trajectories for satellite rendezvous. [Internet] [Masters thesis]. Virginia Tech; 1996. [cited 2020 Sep 27]. Available from: http://hdl.handle.net/10919/41037.

Council of Science Editors:

Kruep JM. Six degree of freedom optimal trajectories for satellite rendezvous. [Masters Thesis]. Virginia Tech; 1996. Available from: http://hdl.handle.net/10919/41037


Delft University of Technology

29. Ardaens, J.H. Angles-only relative navigation in low earth orbit.

Degree: 2020, Delft University of Technology

Rendezvous in orbit has recently regained considerable attention, as it is required to enable on-orbit servicing or active debris removal activities. The pressing need for… (more)

Subjects/Keywords: space rendezvous; angles-only navigation; noncooperative spacecraft

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APA (6th Edition):

Ardaens, J. H. (2020). Angles-only relative navigation in low earth orbit. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:f2947dfb-1482-44f0-8f87-5fa3f5a27b6c ; urn:NBN:nl:ui:24-uuid:f2947dfb-1482-44f0-8f87-5fa3f5a27b6c ; f2947dfb-1482-44f0-8f87-5fa3f5a27b6c ; 10.4233/uuid:f2947dfb-1482-44f0-8f87-5fa3f5a27b6c ; urn:isbn:978-94-028-2153-6 ; urn:NBN:nl:ui:24-uuid:f2947dfb-1482-44f0-8f87-5fa3f5a27b6c ; http://resolver.tudelft.nl/uuid:f2947dfb-1482-44f0-8f87-5fa3f5a27b6c

Chicago Manual of Style (16th Edition):

Ardaens, J H. “Angles-only relative navigation in low earth orbit.” 2020. Doctoral Dissertation, Delft University of Technology. Accessed September 27, 2020. http://resolver.tudelft.nl/uuid:f2947dfb-1482-44f0-8f87-5fa3f5a27b6c ; urn:NBN:nl:ui:24-uuid:f2947dfb-1482-44f0-8f87-5fa3f5a27b6c ; f2947dfb-1482-44f0-8f87-5fa3f5a27b6c ; 10.4233/uuid:f2947dfb-1482-44f0-8f87-5fa3f5a27b6c ; urn:isbn:978-94-028-2153-6 ; urn:NBN:nl:ui:24-uuid:f2947dfb-1482-44f0-8f87-5fa3f5a27b6c ; http://resolver.tudelft.nl/uuid:f2947dfb-1482-44f0-8f87-5fa3f5a27b6c.

MLA Handbook (7th Edition):

Ardaens, J H. “Angles-only relative navigation in low earth orbit.” 2020. Web. 27 Sep 2020.

Vancouver:

Ardaens JH. Angles-only relative navigation in low earth orbit. [Internet] [Doctoral dissertation]. Delft University of Technology; 2020. [cited 2020 Sep 27]. Available from: http://resolver.tudelft.nl/uuid:f2947dfb-1482-44f0-8f87-5fa3f5a27b6c ; urn:NBN:nl:ui:24-uuid:f2947dfb-1482-44f0-8f87-5fa3f5a27b6c ; f2947dfb-1482-44f0-8f87-5fa3f5a27b6c ; 10.4233/uuid:f2947dfb-1482-44f0-8f87-5fa3f5a27b6c ; urn:isbn:978-94-028-2153-6 ; urn:NBN:nl:ui:24-uuid:f2947dfb-1482-44f0-8f87-5fa3f5a27b6c ; http://resolver.tudelft.nl/uuid:f2947dfb-1482-44f0-8f87-5fa3f5a27b6c.

Council of Science Editors:

Ardaens JH. Angles-only relative navigation in low earth orbit. [Doctoral Dissertation]. Delft University of Technology; 2020. Available from: http://resolver.tudelft.nl/uuid:f2947dfb-1482-44f0-8f87-5fa3f5a27b6c ; urn:NBN:nl:ui:24-uuid:f2947dfb-1482-44f0-8f87-5fa3f5a27b6c ; f2947dfb-1482-44f0-8f87-5fa3f5a27b6c ; 10.4233/uuid:f2947dfb-1482-44f0-8f87-5fa3f5a27b6c ; urn:isbn:978-94-028-2153-6 ; urn:NBN:nl:ui:24-uuid:f2947dfb-1482-44f0-8f87-5fa3f5a27b6c ; http://resolver.tudelft.nl/uuid:f2947dfb-1482-44f0-8f87-5fa3f5a27b6c

30. Fonod, Robert. Model-based Fault Diagnosis and Fault Accommodation for Space Missions : Application to the Rendezvous Phase of the MSR Mission : Diagnostique de défaut à base de modèle et accommodation de défaut pour missions spatiales.

Degree: Docteur es, Automatique, productique, signal et image, ingénierie cognitique, 2014, Bordeaux

Les travaux de recherche traités dans cette thèse s’appuient sur l’expertise des actionsmenées entre l’Agence spatiale européenne (ESA), l’industrie Thales Alenia Space (TAS) et le… (more)

Subjects/Keywords: Diagnostic des défauts; Commande tolérante aux défauts rendez-vous spatial; Fault diagnosis; Fault-tolerant control; Space rendezvous

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

APA (6th Edition):

Fonod, R. (2014). Model-based Fault Diagnosis and Fault Accommodation for Space Missions : Application to the Rendezvous Phase of the MSR Mission : Diagnostique de défaut à base de modèle et accommodation de défaut pour missions spatiales. (Doctoral Dissertation). Bordeaux. Retrieved from http://www.theses.fr/2014BORD0199

Chicago Manual of Style (16th Edition):

Fonod, Robert. “Model-based Fault Diagnosis and Fault Accommodation for Space Missions : Application to the Rendezvous Phase of the MSR Mission : Diagnostique de défaut à base de modèle et accommodation de défaut pour missions spatiales.” 2014. Doctoral Dissertation, Bordeaux. Accessed September 27, 2020. http://www.theses.fr/2014BORD0199.

MLA Handbook (7th Edition):

Fonod, Robert. “Model-based Fault Diagnosis and Fault Accommodation for Space Missions : Application to the Rendezvous Phase of the MSR Mission : Diagnostique de défaut à base de modèle et accommodation de défaut pour missions spatiales.” 2014. Web. 27 Sep 2020.

Vancouver:

Fonod R. Model-based Fault Diagnosis and Fault Accommodation for Space Missions : Application to the Rendezvous Phase of the MSR Mission : Diagnostique de défaut à base de modèle et accommodation de défaut pour missions spatiales. [Internet] [Doctoral dissertation]. Bordeaux; 2014. [cited 2020 Sep 27]. Available from: http://www.theses.fr/2014BORD0199.

Council of Science Editors:

Fonod R. Model-based Fault Diagnosis and Fault Accommodation for Space Missions : Application to the Rendezvous Phase of the MSR Mission : Diagnostique de défaut à base de modèle et accommodation de défaut pour missions spatiales. [Doctoral Dissertation]. Bordeaux; 2014. Available from: http://www.theses.fr/2014BORD0199

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