Lift control system for aircraft vertical path guidance

Details Lift control system for aircraft vertical path guidance Lift control system for aircraft vertical path guidance

1980-03-31

1982-04-20

Nusbaum, Mark E.

Boots, shoes, and leggings

364428, 244181, 73178T, G06G 778

Patent

active

043262538

ABSTRACT:
A system for providing an optimum lift demand signal for aircraft maneuvers such as "go-around" includes a computer for generating a reference angle of attack signal which is functionally related to the aircraft's vertical velocity. The reference signal is compared with a signal corresponding to the aircraft's actual angle of attack, thereby producing an error signal. The error signal is utilized as a control to the aircraft's dynamics for optimizing the aircraft's climb-out performance.

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