Aircraft flight command and display system

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364428, 364435, 340968, 73178T, 244181, G06F 1550

Patent

active

047632666

ABSTRACT:
A system particularly adapted for guiding aircraft through wind shear conditions includes: a thrust command control (10) for maintaining airspeed and groundspeed within a defined range; a detection system (12) for detecting and annunciating the presence of moderate and severe wind shear; and a pitch command system (14) which provides pitch command signals for optimum climb out from a wind shear condition.

REFERENCES:
patent: 3618002 (1971-11-01), Stinson
patent: 3860800 (1975-01-01), Simpson
patent: 4021010 (1977-05-01), Bliss
patent: 4129275 (1978-12-01), Gerstine et al.
patent: 4189118 (1980-02-01), Peter-Contesse
patent: 4319219 (1982-03-01), Rein-Weston
patent: 4326253 (1982-04-01), Cooper et al.

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