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Overview and Software Architecture of the Copernicus Trajectory Design and Optimization SystemThe Copernicus Trajectory Design and Optimization System represents an innovative and comprehensive approach to on-orbit mission design, trajectory analysis and optimization. Copernicus integrates state of the art algorithms in optimization, interactive visualization, spacecraft state propagation, and data input-output interfaces, allowing the analyst to design spacecraft missions to all possible Solar System destinations. All of these features are incorporated within a single architecture that can be used interactively via a comprehensive GUI interface, or passively via external interfaces that execute batch processes. This paper describes the Copernicus software architecture together with the challenges associated with its implementation. Additionally, future development and planned new capabilities are discussed. Key words: Copernicus, Spacecraft Trajectory Optimization Software.
Document ID
20100017807
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Williams, Jacob
(Engineering Research and Consulting, Inc. Houston, TX, United States)
Senent, Juan S.
(Odyssey Space Research, LLC Houston, TX, United States)
Ocampo, Cesar
(Texas Univ. Austin, TX, United States)
Mathur, Ravi
(Texas Univ. Austin, TX, United States)
Davis, Elizabeth C.
(Jacobs Technologies Engineering Science Contract Group Houston, TX, United States)
Date Acquired
August 29, 2013
Publication Date
May 3, 2010
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Report/Patent Number
JSC-CN-20553
Meeting Information
Meeting: 4th International Conference on Astrodynamics Tools and Techniques
Location: Madrid
Country: Spain
Start Date: May 3, 2010
End Date: May 6, 2010
Sponsors: European Space Astronomy Centre (ESAC)
Distribution Limits
Public
Copyright
Public Use Permitted.
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