Patent · US Active

Method and device for aiding the control of guiding modes transitions of an aircraft

US8731744B2 · kind B2 · utility

0Cited by
10References
11Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJul 14, 2011
Grant dateMay 20, 2014
Priority date
Expiry dateMay 12, 2033

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG05D1/085
  • WIPO fieldControl
  • WIPO sectorInstruments

Abstract

The guiding mode transition aiding device includes a target heading determining device and a mode transition triggering system. The target heading determining device is configured to determine a target heading which represents the heading value reached by the aircraft at the end of a procedure of folding the wings of the aircraft flat from a current operating state. The mode transition triggering system receives the target heading and compares the target heading to a desired heading to be reached by the airplane to assist with triggering a transition between a rolling angle holding mode, in which the aircraft flies with a constant rolling angle, to a heading holding mode, in which the aircraft flies with a constant heading. This device and associated methods may be used during in flight refueling operations.

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