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 |