Stabilization control circuit for vertical position in an inerti

Details Stabilization control circuit for vertical position in an inerti Stabilization control circuit for vertical position in an inerti

1987-04-16

1989-11-21

Chin, Gary

Boots, shoes, and leggings

364433, G06F 1550

Patent

active

048826979

ABSTRACT:
Vertical velocity and vertical position of an aircraft are derived from the vertical acceleration and a measurement of altitude based on barometric pressure. An acceleration correction signal and a velocity correction signal are derived from an altitude error signal and the rate of change of altitude based on the barometric altimeter. The acceleration correction signal and velocity correction signal functions are such that the acceleration correction signal and the velocity correction signal are responsive to rapid climbs and dives of the aircraft.

REFERENCES:
patent: 4106094 (1978-08-01), Land
patent: 4495580 (1985-01-01), Keearns
patent: 4538230 (1985-08-01), Reust et al.
"Optimizing the Gains of the Baro-Inertial Vertical Channel", by Widnall, Annual of Guidance and Control, vol. 3 (1980), Mar.-Apr., No. 2, New York.

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