| 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 |