Fly-by-wire control system for an aircraft comprising detection of pilot induced oscillations and a control for such a system
US8473121B2 · kind B2 · utility
2Cited by
15References
8Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Apr 22, 2010 |
| Grant date | Jun 25, 2013 |
| Priority date | — |
| Expiry date | Apr 27, 2030 |
Classification
- Technology area (CPC G)Physics
- CPC primaryG05D1/0816
- WIPO fieldControl
- WIPO sectorInstruments
Abstract
A fly-by-wire control system for an aircraft including detection of pilot induced oscillations and a mobile control unit for such a system. According to the invention, provision is made for the pivotings of the mobile control unit to be damped by a controllable damper controlled by a detector that detects oscillations corresponding to pilot induced oscillations.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.