System, method, and apparatus for control input prediction...

Power plants – Reaction motor – With thrust direction modifying means

Reexamination Certificate

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C060S228000, C239S265170, C239S265190

Reexamination Certificate

active

08065868

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.

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