Patent · US Active

System, method, and apparatus for control input prediction and state verification of fluidic vectoring exhaust in high performance aircraft

US8065868B2 · kind B2 · utility

0Cited by
9References
14Claims
0Family size

Assignee

Inventors

Key dates

Filing dateDec 22, 2006
Grant dateNov 29, 2011
Priority date
Expiry dateSep 28, 2030

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF05D2270/301
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A non-invasive system, method, and apparatus for control input prediction and state verification of an aircraft's fluidic vectoring exhaust is disclosed. The control system derives a desired vector state, then predicts and sets the fluidic injection input required to produce the desired vector state. A vectored state verification routine is used to determine the resulting vector state for feedback to the control system.

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