Velocity damped erection system for stable gyroscopic attitude a

Details Velocity damped erection system for stable gyroscopic attitude a Velocity damped erection system for stable gyroscopic attitude a

1975-03-17

1976-09-07

Kunin, Stephen G.

Aeronautics and astronautics

Aircraft control

Automatic

33321, 73178R, 74 534, 74 547, 23515025, 244191, 318649, 31851, G05D 100, B64C 1318

Patent

active

039790908

ABSTRACT:
An improved second order gyroscopic attitude and heading reference system including separate variable time constant accelerometer integrators for independently controlling the velocity error signals associated with respective east and north acceleration signals to provide velocity damped output signals so that a high acceleration input signal of dubious accuracy will have minimal precessional authority while a lower acceleration input signal of greater accuracy will retain nominal control.

REFERENCES:
patent: 2995318 (1961-08-01), Cocharo
patent: 3028592 (1962-04-01), Parr et al.
patent: 3167763 (1965-01-01), Barkalow et al.
patent: 3648525 (1972-03-01), Reed

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