Patent · US Active

Automatic trim system for fly-by-wire aircraft with unique trim controllers

US8231085B2 · kind B2 · utility

12Cited by
41References
17Claims
0Family size

Assignee

Inventor

Key dates

Filing dateApr 8, 2010
Grant dateJul 31, 2012
Priority date
Expiry dateJan 31, 2031

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG05D1/0858
  • WIPO fieldControl
  • WIPO sectorInstruments

Abstract

A flight control system includes a controller which defines a controller displacement and a control surface which defines a control surface authority. A module operable to provide a displacement feel to the controller in response to a remaining portion of the controller displacement being greater than a remaining portion of the control surface authority and the module operable to re-reference a center of the controller displacement to equate the remaining portion of the controller displacement with the remaining portion of the control surface authority in response to the remaining portion of the controller displacement being less than the remaining portion of the control surface authority.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.