NDLI: Attitude determination improvements for goes

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Attitude determination improvements for goes

Content Provider	NASA Technical Reports Server (NTRS)
Author	Kyle, Arthur M. Markley Sr., F. Landis Kull, Kathie Crassidis, John L.
Copyright Year	1996
Description	In this paper, a summary of the basic simulation parameters and results of a new study for the Geostationary Operational Environmental Satellite (GOES) is shown. The study for GOES involves the simulation of minor modifications to the current spacecraft, so that the relative performance of these modifications can be analyzed. The first modification studies requires the placement of a baseline inertial reference unit, such as the Dry Rotor Inertial Reference Unit or the Hemispherical Resonator Gyro onto the spacecraft. The imager/sounder assembly is currently used to obtain landmark and/or star observations in order to compensate for spacecraft motion and external disturbances through ground processing. The study uses the imager/sounder assembly as another attitude sensor for on-board attitude determination. Also the addition of star trackers is used to provide precise attitude knowledge.
File Size	903657
Page Count	16
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19960035760
Archival Resource Key	ark:/13960/t4xh4j67n
Language	English
Publisher Date	1996-05-01
Access Restriction	Open
Subject Keyword	Astrodynamics Goes Satellites Attitude Inclination Satellite Attitude Control Star Trackers Clouds Meteorology Landmarks Mathematical Models Angular Velocity Sky Brightness Inertial Guidance Gyroscopes Spacecraft Motion Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Article

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