Process and device for estimating the altitude of an aircraft in

Measuring and testing – Navigation – Take-off and landing monitors

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73178T, 340977, 364433, G01C 2116

Patent

active

054150310

ABSTRACT:
The invention is a process and a device for determining an estimation of the altitude of an aircraft from at least two independent measurements of the altitude, by polling. The aircraft must include at least one inertial reference system. A signal representing a first or second derivative of the altitude is diverted from the inertial reference system, polling is undertaken on the magnitudes of like order deduced from the independent altitude measurements and from the derivative of the altitude, respectively, and an integration operation is undertaken so as to obtain the altitude estimation.

REFERENCES:
patent: 3296422 (1967-01-01), Rusler
patent: 5136512 (1992-08-01), Le Borne
patent: 5233542 (1993-08-01), Hohner et al.
Clark et al., IEEE Trans. on Aero. and Elect. Systems, vol. AES12, (Jul. 4, 1976), pp. 459-463.

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