|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||060/231; 060/228; 239/26517; 239/26519|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 9|
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.
What is claimed is: 1. An aircraft, comprising:a flight control system for controlling flight of the aircraft, including an engine for producing an engine flow, a nozzle having an axis and located downstream from the engine for releasing an exhaust plume from the engine;a fluidic vectoring controller responsive to the flight control system for vectoring the exhaust plume relative to the nozzle in a desired off-axis vector direction; the fluidic vectoring controller controlling:a fluidic off-take system for bleeding off a portion of the engine flow, the f...