Autopilot system for a helicopter
US7558653B2 · kind B2 · utility
1Cited by
23References
5Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Oct 11, 2005 |
| Grant date | Jul 7, 2009 |
| Priority date | — |
| Expiry date | Dec 24, 2025 |
Classification
- Technology area (CPC G)Physics
- CPC primaryG05D1/102
- WIPO fieldControl
- WIPO sectorInstruments
Abstract
The present invention relates to an autopilot system for a rotary wing aircraft operating relative to at least two pilot axes, which system comprises, for each of the two axes, at least one servo-control relationship providing a respective initial control instruction, with the two relationships having a common target; the system includes combination means (36) for providing a series of control instructions by combining the two initial control instructions (UCV, UTV).
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.