http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CA-2080609-A1

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filingDate 1992-10-15-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_39cd1af9d31ed2a0bf0311079e7376cd
publicationDate 1993-05-28-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber CA-2080609-A1
titleOfInvention Method and apparatus for controlling a solar wing of a satellite using a sun sensor
abstract METHOD AND APPARATUS FOR CONTROLLING A SOLAR WING OF A SATELLITE USING A SUN SENSOR ABSTRACT OF THE DISCLOSURE This invention discloses a method for maintaining a desirable orientation of the solar wings of an orbiting satellite (103 relative to the sun. A dual array of sun sensors (26,28) is positioned on a body (12) of the satellite (10) in order to get a measurement of the position of the sun relative to the body (12) once per every orbit of the satellite (10). In addition, an estimate of the position of the solar wings (16, 17) relative to the body (12) of the satellite (10) is attained. The sun to-body angle is then subtracted from the body-to-wing angle to drive an error signal which is applied to a wing driver mechanism in order to maintain the solar wings (16,17) of the satellite (10) in a proper orientation relative to the sun.
priorityDate 1991-11-27-04:00^^<http://www.w3.org/2001/XMLSchema#date>
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Total number of triples: 27.