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MeetingACGS Committee Meeting 107 - Boulder - March 2011
Agenda Location5 SUBCOMMITTEE B – MISSILES AND SPACE
5.1 Kepler Attitude Control and Determination System Overview and Early Mission Experiences
TitleKepler Attitude Control and Determination System Overview and Early Mission Experiences
PresenterDustin Putnam
AffiliationBall Aerospace
Available Downloads*presentation
*Downloads are available to members who are logged in and either Active or attended this meeting.
AbstractDustin Putnam
Ball Aerospace

Abstract

The Kepler spacecraft was launched on March 7, 2009. Designed and built for NASA by Ball Aerospace & Technologies Corp., the Kepler mission uses the transit method to detect Earth-like exoplanets – approximately Earth-sized planets that are in the habitable zone of their stars.
Kepler, the largest telescope ever launched beyond Earth orbit, is in a heliocentric, Earth-trailing, drift-away orbit. It is a 3-axis stabilized, inertially-fixed pointer, using a combination of sun sensors, star trackers, inertial measurement units, and fine guidance sensors for attitude determination and reaction wheels and hydrazine thrusters for attitude and momentum control. This paper presents an overview of the Kepler mission, the ADCS design and some early mission experiences.



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