Aircraft stabilizing system

Aeronautics and astronautics – Aircraft – steering propulsion – Fluid

Patent

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Details

244 76R, B64B 136

Patent

active

056012560

ABSTRACT:
A system for stabilizing an aircraft includes sensors positioned and disposed at predetermined locations on the aircraft and structured for sensing external forces acting on the aircraft at the sensor locations as a result of rapid changes in atmospheric conditions such as those associated with air turbulence and wind shear. A computer processor receives data from the sensors and activates one or more thrust generators positioned at predetermined locations of the aircraft to counteract the external forces and maintain the desired attitude and stability of the aircraft.

REFERENCES:
patent: 2395435 (1946-02-01), Thompson et al.
patent: 3008672 (1961-11-01), Moore et al.
patent: 3210937 (1965-10-01), Perry
patent: 4648569 (1987-03-01), Stewart

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