Inertial flight director system

Details Inertial flight director system Inertial flight director system

1984-02-15

1985-08-06

Gruber, Felix D.

Boots, shoes, and leggings

364429, 364430, 244186, G05D 112, G06G 770, B64C 1318

Patent

active

045340005

ABSTRACT:
The disclosed apparatus is useful in controlling an aircraft inertial flight path on the final approach to landing to coincide with a desired flight path represented by the intersection of the localizer and glide path electronic beam signals, and there being an inertially responsive unit on the aircraft.
The apparatus includes:

REFERENCES:
patent: 3618002 (1971-11-01), Stinson
patent: 3927306 (1975-12-01), Miller
patent: 3964053 (1976-06-01), Heiser
patent: 4004758 (1977-01-01), Boriss et al.
patent: 4021010 (1977-05-01), Bliss
patent: 4133503 (1979-01-01), Bliss
patent: 4141522 (1979-02-01), Lambregts
patent: 4357661 (1982-11-01), Lambregts et al.
MacKinnon: Improving Automatic Landing System Performance Using Modern Control Theory and Inertial Measurements, Jan. 1969, MIT Instrumentation Laboratory Report.
Gelb et al.: Applied Optimal Estimation, the MIT Press, 1974, Cambridge MA.

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