Method and system for ensuring the reliability of data used to p

Boots – shoes – and leggings

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318563, 318564, 244195, 36442401, G06F 1100, G06F 1116

Patent

active

053351770

ABSTRACT:
The disclosure relates to systems for piloting aircraft. Equations of the movements of the aircraft are used for computing, in a computer, of the first and second derivatives parameters V.sub.p, .PHI..sub.v, .sigma..sub.a, .beta..sub.v, .alpha., .PHI..sub.v, .sigma..sub.a, .beta..sub.v, of the parameters V.sub.p, .PHI..sub.v, .sigma..sub.a, .beta..sub.v, .alpha. of the movement of the aircraft, and the values thus computed are compared with those computed by means of the values of said parameters V.sub.p, .PHI..sub.v, .sigma..sub.a, .beta..sub.v, .alpha. at the instants t, (t+dt) and (t+2dt). An alarm signal (circuit 23) is generated if equality is not verified to a given precision.

REFERENCES:
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patent: 4032757 (1977-06-01), Eccles
patent: 4101958 (1978-07-01), Patterson et al.
patent: 4327437 (1982-04-01), Gelderloos
patent: 4698785 (1987-10-01), Desmond et al.
patent: 5079707 (1992-01-01), Bird et al.
patent: 5222065 (1993-06-01), Krogmann
Daniel M. Wilbers et al, "Detection Filters for Aircraft Sensor and Actuator Faults", ICCON '89 IEEE International Conference on Control and Applications, Apr. 1989, pp. 1-6, (p. 3 paragraph 4 & p. 4 paragraph 4.3).

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