The Resource Guidance, navigation and control system for autonomous proximity operations and docking of spacecraft, by Daero Lee, (electronic resource)
Guidance, navigation and control system for autonomous proximity operations and docking of spacecraft, by Daero Lee, (electronic resource)
Resource Information
The item Guidance, navigation and control system for autonomous proximity operations and docking of spacecraft, by Daero Lee, (electronic resource) represents a specific, individual, material embodiment of a distinct intellectual or artistic creation found in Missouri University of Science & Technology Library.This item is available to borrow from all library branches.
Resource Information
The item Guidance, navigation and control system for autonomous proximity operations and docking of spacecraft, by Daero Lee, (electronic resource) represents a specific, individual, material embodiment of a distinct intellectual or artistic creation found in Missouri University of Science & Technology Library.
This item is available to borrow from all library branches.
- Summary
- "This study develops an integrated guidance, navigation and control system for use in autonomous proximity operations and docking of spacecraft. A new approach strategy is proposed based on a modified system developed for use with the International Space Station. It is composed of three "V-bar hops" in the closing transfer phase, two periods of stationkeeping and a "straight line V-bar" approach to the docking port. Guidance, navigation and control functions are independently designed and are then integrated in the form of linear Gaussian-type control. The translational maneuvers are determined through the integration of the state-dependent Riccati equation control formulated using the nonlinear relative motion dynamics with the weight matrices adjusted at the steady state condition. The reference state is provided by a guidance function, and the relative navigation is performed using a rendezvous laser vision system and a vision sensor system, where a sensor mode change is made along the approach in order to provide effective navigation. The rotational maneuvers are determined through a linear quadratic Gaussian-type control using star trackers and gyros, and a vision sensor. The attitude estimation mode change is made from absolute estimation to relative attitude estimation during the stationkeeping phase inside the approach corridor. The rotational controller provides the precise attitude control using weight matrices adjusted at the steady state condition, including the uncertainty of the moment of inertia and external disturbance torques. A six degree-of-freedom simulation demonstrates that the newly developed GNC system successfully autonomously performs proximity operations and meets the conditions for entering the final docking phase"--Abstract, p. iii
- Language
- eng
- Extent
- 1 online resource (x, 137 pages)
- Note
-
- Vita
- The entire thesis text is included in file
- Title from title screen of thesis/dissertation PDF file (viewed September 8, 2011)
- Label
- Guidance, navigation and control system for autonomous proximity operations and docking of spacecraft
- Title
- Guidance, navigation and control system for autonomous proximity operations and docking of spacecraft
- Statement of responsibility
- by Daero Lee
- Language
- eng
- Summary
- "This study develops an integrated guidance, navigation and control system for use in autonomous proximity operations and docking of spacecraft. A new approach strategy is proposed based on a modified system developed for use with the International Space Station. It is composed of three "V-bar hops" in the closing transfer phase, two periods of stationkeeping and a "straight line V-bar" approach to the docking port. Guidance, navigation and control functions are independently designed and are then integrated in the form of linear Gaussian-type control. The translational maneuvers are determined through the integration of the state-dependent Riccati equation control formulated using the nonlinear relative motion dynamics with the weight matrices adjusted at the steady state condition. The reference state is provided by a guidance function, and the relative navigation is performed using a rendezvous laser vision system and a vision sensor system, where a sensor mode change is made along the approach in order to provide effective navigation. The rotational maneuvers are determined through a linear quadratic Gaussian-type control using star trackers and gyros, and a vision sensor. The attitude estimation mode change is made from absolute estimation to relative attitude estimation during the stationkeeping phase inside the approach corridor. The rotational controller provides the precise attitude control using weight matrices adjusted at the steady state condition, including the uncertainty of the moment of inertia and external disturbance torques. A six degree-of-freedom simulation demonstrates that the newly developed GNC system successfully autonomously performs proximity operations and meets the conditions for entering the final docking phase"--Abstract, p. iii
- Cataloging source
- UMR
- http://library.link/vocab/creatorDate
- 1974-
- http://library.link/vocab/creatorName
- Lee, Daero
- Degree
- Ph. D.
- Dissertation year
- 2009.
- Granting institution
- Missouri University of Science and Technology
- Illustrations
- illustrations
- Index
- no index present
- Literary form
- non fiction
- Nature of contents
-
- dictionaries
- bibliography
- theses
- http://library.link/vocab/subjectName
-
- Space vehicles
- Navigation (Astronautics)
- Orbital rendezvous (Space flight)
- Couplings
- Autonomy
- Target audience
- specialized
- Label
- Guidance, navigation and control system for autonomous proximity operations and docking of spacecraft, by Daero Lee, (electronic resource)
- Note
-
- Vita
- The entire thesis text is included in file
- Title from title screen of thesis/dissertation PDF file (viewed September 8, 2011)
- Bibliography note
- Includes bibliographical references (pages 128-136)
- Carrier category
- online resource
- Carrier category code
-
- cr
- Carrier MARC source
- rdacarrier
- Color
- black and white
- Content category
- text
- Content type code
-
- txt
- Content type MARC source
- rdacontent
- Control code
- 750547206
- Dimensions
- unknown
- Extent
- 1 online resource (x, 137 pages)
- Form of item
- electronic
- Media category
- computer
- Media MARC source
- rdamedia
- Media type code
-
- c
- Other physical details
- illustrations, digital, PDF file.
- Specific material designation
- remote
- System control number
- (OCoLC)750547206
- System details
-
- System requirements: Adobe Acrobat Reader; Internet browser
- Mode of access: World Wide Web
- Label
- Guidance, navigation and control system for autonomous proximity operations and docking of spacecraft, by Daero Lee, (electronic resource)
- Note
-
- Vita
- The entire thesis text is included in file
- Title from title screen of thesis/dissertation PDF file (viewed September 8, 2011)
- Bibliography note
- Includes bibliographical references (pages 128-136)
- Carrier category
- online resource
- Carrier category code
-
- cr
- Carrier MARC source
- rdacarrier
- Color
- black and white
- Content category
- text
- Content type code
-
- txt
- Content type MARC source
- rdacontent
- Control code
- 750547206
- Dimensions
- unknown
- Extent
- 1 online resource (x, 137 pages)
- Form of item
- electronic
- Media category
- computer
- Media MARC source
- rdamedia
- Media type code
-
- c
- Other physical details
- illustrations, digital, PDF file.
- Specific material designation
- remote
- System control number
- (OCoLC)750547206
- System details
-
- System requirements: Adobe Acrobat Reader; Internet browser
- Mode of access: World Wide Web
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<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.library.mst.edu/portal/Guidance-navigation-and-control-system-for/La6CSqLQ8Go/" typeof="Book http://bibfra.me/vocab/lite/Item"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.library.mst.edu/portal/Guidance-navigation-and-control-system-for/La6CSqLQ8Go/">Guidance, navigation and control system for autonomous proximity operations and docking of spacecraft, by Daero Lee, (electronic resource)</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.library.mst.edu/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.library.mst.edu/">Missouri University of Science & Technology Library</a></span></span></span></span></div>
