Self-aligning roll out guidance system

Details Self-aligning roll out guidance system Self-aligning roll out guidance system

1975-07-10

1977-02-08

Kunin, Stephen G.

Aeronautics and astronautics

Aircraft control

Automatic

23515022, G05D 112

Patent

active

040068706

ABSTRACT:
Guidance along the runway centerline when visibility conditions do not permit adequate visual cues for manual control are provided utilizing lateral acceleration and bank angle information. An aircraft type airborne vehicle can touchdown with a crab angle in the presence of a crosswind and the present system provides the proper command to decrab the aircraft and return the aircraft to the centerline.

REFERENCES:
patent: 2827250 (1958-03-01), Rusler, Jr.
patent: 2948495 (1960-08-01), Maregraf
patent: 3110458 (1963-11-01), Bishop
patent: 3136502 (1964-06-01), Auld, Jr. et al.
patent: 3223363 (1965-12-01), Boothby et al.
patent: 3843077 (1974-10-01), Boone et al.

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