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CNES Approaching Guidance Experiment within FFIORDThis article outlines the relative orbit control (guidance algorithm and its preliminary performance tests evaluation) that will be tested by the CNES Team on FFIORD (Formation Flying In Orbit Ranging Demonstration) onboard PRISMA mission. After a brief summary of the PRISMA mission context, the paper provides a full description of the rendezvous function involved in the approaching guidance experiment. This FFIORD onboard function is detailed in terms of on-board algorithmic method (basic algorithm and enhanced alternative), sensibility analysis used to construct maneuver plans and preliminary tests results.
Document ID
20080012645
Document Type
Conference Paper
Authors
Berges, Jean-Claude (Centre National d'Etudes Spatiales Toulouse, France)
Cayeux, Philippe (EADS Astrium Ltd. Toulouse, France)
Gaudel-Vacaresse, Angelique (Centre National d'Etudes Spatiales Toulouse, France)
Meyssignac, Benoit (Centre National d'Etudes Spatiales Toulouse, France)
Date Acquired
August 24, 2013
Publication Date
September 24, 2007
Publication Information
Publication: Proceedings of the 20th International Symposium on Space Flight Dynamics
Subject Category
Spacecraft Design, Testing and Performance
Distribution Limits
Public
Copyright
Public Use Permitted.

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IDRelationTitle20080012629Analytic PrimaryProceedings of the 20th International Symposium on Space Flight Dynamics