Digital flight guidance system

Excavating

Patent

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244194, 318564, 364101, 364119, G06F 1550, G06F 1108

Patent

active

042174864

ABSTRACT:
A digital flight guidance system includes a pair of processors, each with its own memory means and arranged with common input and output means for providing monitored guidance of an aircraft when the craft is in cruise modes or when the craft is performing a critical maneuver such as landing, terrain following, or the like.

REFERENCES:
patent: 3517174 (1970-06-01), Ossfeldt
patent: 3688099 (1972-08-01), Buscher
patent: 3770948 (1973-11-01), Caputo et al.
patent: 4030074 (1977-06-01), Giorcelli
patent: 4032757 (1977-06-01), Eccles
patent: 4035705 (1977-07-01), Miller
patent: 4096989 (1978-06-01), Tawfik
patent: 4101958 (1978-07-01), Patterson et al.
patent: 4115847 (1978-09-01), Osder et al.
patent: 4130241 (1978-12-01), Meredith et al.
DiPilato: IBM Technical Disclosure Bull., vol. 18, No. 12, May 1976, pp. 4040/4041, Synchronization of Two Controllers.

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