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ATTITUDE SENSOR
   
Document Number
US Patent 3780966
Issued Date
December 25, 1973
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Abstract
The invention consists essentially of two light sensors on a spacecraft that are mounted beneath a baffle which divides the light from a light source such as the sun or a star. The divided light reflects off of two reflective surfaces onto the two light sensors. When the spacecraft assumes its normal attitude the baffle divides the light from the light source into two equal parts cuasing the two light sensors to produce equal outputs. An electrical circuit containing the two sensors produces a zero voltage output when the outputs of the two light sensors are equal thereby indicating that the spacecraft is in its normal attitude relative to the light source. While the spacecraft is not in its normal attitude relative to the light source the two light sensors produce unequal outputs causing the electrical circuit to produce an output voltage. The amplitude and polarity of this output voltage are indicative of the attitude of the spacecraft and can be applied to the controls of the spacecraft to return it to its normal attitude.
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ATTITUDE SENSOR - US Patent 3780966 Drawing
Drawing from US Patent 3780966
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Number of Claims:
5
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Published
December 25, 1973
Application Number
05/289,049
Filed
September 14, 1972
US Classification
244/171   244/3.16 250/203.6 250/237R
Int'l Classification
B64G   1/36   (20060101)  
Examiner
Assistant Examiner
USPTO Field of Search
244/1SS   244/1SA   244/321   244/3.16   250/23R   250/228   250/237R   318/313   318/480   318/580  
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Description
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