A pyramid skewed axis sensor set for multiplex flight control systems

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dc.contributor.author D. Kimberley en_US
dc.date.accessioned 2014-10-21T15:51:31Z
dc.date.available 2014-10-21T15:51:31Z
dc.date.issued 1975 en_US
dc.identifier.other ARC/R&M-3808 en_US
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/3089
dc.description.abstract In order to meet the 'two defect survival' capability in future full-time flight control systems, one approach is to use four identical sensors in each axis, giving a total of twelve for a three-axis system. An alternative eight Sensor Pyramid Arrangement has been developed which offers a similar 'two defect survival' capability in all three axes leading to reduced cost and maintenance effort but with slightly larger transients following failure of a sensor. The pyramid arrangement can also be used for 'fail safe' systems reducing the number of sensors from six to four, or alternatively for a twelve gyro, 'four defect survival' configuration. en_US
dc.relation.ispartofseries Aeronautical Research Council Reports & Memoranda en_US
dc.title A pyramid skewed axis sensor set for multiplex flight control systems en_US


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