Space station GN&C overview for payloads

Details Space station GN&C overview for payloads Space station GN&C overview for payloads

Jan 1999

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1999aipc..458...49t&link_type=abstract

Space technology and applications international forum -1999. AIP Conference Proceedings, Volume 458, pp. 49-57 (1999).

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Spaceborne And Space Research Instruments, Apparatus, And Components

Scientific paper

The Guidance, Navigation, and Control (GN&C) function on the International Space Station (ISS) determines navigation parameters (state vector, attitude, angular rate, pointing data, time), maintains Station attitude (non propulsively as a rule but propulsively when necessary), executes translation and reboost maneuvers, and supports microgravity experiments by limiting accelerations. The accuracies to which GN&C is to perform its functions are summarized, and then the expected performance of the current GN&C design is described, including pointing accuracy. Attitude bounds are illustrated as a function of calendar date given the current (Revision D) station assembly sequence and schedule.

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