Helicopter control systems

Details Helicopter control systems Helicopter control systems

1989-03-27

1990-08-07

Lall, Parshotam S.

Boots, shoes, and leggings

364434, 36443101, 244 1713, G06F 1516

Patent

active

049473344

ABSTRACT:
A helicopter control system comprises a flight control computer, an engine control computer and an integrated flight and engine control computer, the latter generating output signals operative both in a flight control system and an engine control system to eliminate or reduce transient variations in the speed of rotation of a main sustaining rotor. The invention can be used with full or limited authority flight control systems.

REFERENCES:
patent: 4109886 (1978-08-01), Tribken et al.
patent: 4217486 (1980-08-01), Tawfik et al.
patent: 4313201 (1982-01-01), Fischer et al.
patent: 4500966 (1985-02-01), Zagranski et al.
patent: 4807129 (1989-02-01), Perks

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