DocumentCode
3207723
Title
Relative orbit design tool
Author
Tollefson, Mark V.
Author_Institution
Dynacs, Inc., Albuquerque, NM, USA
Volume
7
fYear
2001
fDate
2001
Firstpage
7
Abstract
A software tool was developed to facilitate the design of sets of satellite orbits such that the satellites always remain in close proximity to one another. The group of satellites is typically referred to as a cluster, and the close proximity motions are often termed formation flying. Such relative motion is well understood only for near-circular orbits, and no method existed to easily and rapidly design a cluster and compute the orbital parameters for the individual satellites. This tool provides that functionality with a graphical user interface to allow almost anyone to easily design and analyze relative orbits. The tool has several additional capabilities. It displays close-approach information for collision detection. It displays the relative orbits using a two-body orbit propagator so the effects of elliptical orbits can be studied. It exports the orbital data in several formats to facilitate further analysis
Keywords
CAD; aerospace computing; artificial satellites; engineering graphics; graphical user interfaces; rotation; GUI; close proximity motions; close-approach information; collision detection; coordinate system; elliptical orbits; formation flying; graphical user interface; orbital parameters; relative motion; relative orbit design tool; satellite orbit design; satellites cluster; software tool; two-body orbit propagator; Aperture antennas; Displays; Earth; Equations; Graphical user interfaces; Radar antennas; Satellite antennas; Software tools; Spaceborne radar; Synthetic aperture radar;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2001, IEEE Proceedings.
Conference_Location
Big Sky, MT
Print_ISBN
0-7803-6599-2
Type
conf
DOI
10.1109/AERO.2001.931425
Filename
931425
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