Method and a system for determining an angular velocity in turning for a rotary wing aircraft
US9493234B2 · kind B2 · utility
0Cited by
6References
15Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Dec 10, 2015 |
| Grant date | Nov 15, 2016 |
| Priority date | — |
| Expiry date | Dec 10, 2035 |
Classification
- Technology area (CPC G)Physics
- CPC primaryG05D1/0858
- WIPO fieldControl
- WIPO sectorInstruments
Abstract
A method and a system for determining an angular velocity in turning for a rotary wing aircraft in order to make turns that are coordinated relative to the ground or else relative to the air and in order to manage the transition between ground coordination and air coordination while taking account of the wind to which the aircraft is subjected. The method serving to determine an angular velocity in yaw using an anticipation value and a correction value on the basis in particular of speeds of advance of the aircraft relative to the ground and relative to the air of its lateral acceleration and of its lateral load factor.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.