Apparatus for determining the position of an aircraft with respe

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244183, 364426, G05D 106, G06F 1550

Patent

active

043162525

ABSTRACT:
Upon landing approach to a runway, glideslope and altitude information is processed to produce an indication of ground distance to the touchdown point. Actual aircraft position is then determined by integrating the aircraft's ground speed. A display of distance from the beginning and end of the runway is provided. An alert is produced if the aircraft approaches the end of the runway at excessive speed. Further, the system may be coupled to the aircraft's autobrake system to automatically control the rate of deceleration.

REFERENCES:
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patent: 3382351 (1968-05-01), Schweighofer et al.
patent: 3644722 (1972-02-01), Hobbs et al.
patent: 3868497 (1975-02-01), Vietor
patent: 3979057 (1976-09-01), Katz et al.
patent: 4147056 (1979-04-01), Muller
patent: 4156912 (1979-05-01), Shigeta et al.
patent: 4172285 (1979-10-01), Yoshida et al.

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