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Formation acquisition sensor for the Terrestrial Planet Finder (TPF) mission

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dc.contributor.author Tien, Jeffrey Y.
dc.contributor.author Srinivasan, Jeffrey M.
dc.contributor.author Young, Larry E.
dc.contributor.author Purcell, George H. Jr.
dc.date.accessioned 2006-02-01T20:43:26Z
dc.date.available 2006-02-01T20:43:26Z
dc.date.issued 2004-03-06
dc.identifier.citation 2004 IEEE Aerospace Conference, Big Sky, Montana, March 6-13, 2004 en
dc.identifier.clearanceno 03-2992
dc.identifier.uri http://hdl.handle.net/2014/38409
dc.description.abstract The Terrestrial Planet Finder (TPF) pre-project, an element of NASA’s Origins Program, is currently investigating multiple implementation architectures for finding earth-like planets around other stars. One of the technologies being developed is the Formation Flying Interferometer (FFI). The FFI is envisioned to consist of up to seven spacecraft, each with an infrared telescope, flying in precise formation within +/- l cm of pre-determined trajectories for synchronized observations. The spacecraft to- spacecraft separations are variable between 20 m to 100m during observations to support various interferometer configurations in the planet-finding mode. The challenges involved with TPF autonomous operations, ranging from formation acquisition and formation maneuvering, to high precision formation flying during science observations are unprecedented for deep space missions. To meet these challenges, the Formation Sensor Testbed (FST) under the TPF technology program will develop and demonstrate the key technology of the formation acquisition sensor. Key performance targets for the acquisition sensor are an instantaneous 4phi-steradian field of view and simultaneous range and bearing-angle measurements for multiple spacecraft with accuracy better than 50 cm and 1 degree, respectively. In this paper, we will describe the TPF FFI mission concept, the key formation flying challenges, the acquisition sensor design, the key design challenges, and the current plan to mitigate these design challenges. en
dc.description.sponsorship NASA/JPL en
dc.format.extent 4599396 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US en
dc.publisher Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2004 en
dc.subject Terrestrial Planet Finder (TPF) en
dc.subject formation flying en
dc.subject formation flying sensor en
dc.title Formation acquisition sensor for the Terrestrial Planet Finder (TPF) mission en
dc.type Preprint en


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