Proactive optical trajectory following system

Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance

Reexamination Certificate

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Details

C244S003150, C356S342000, C250S372000

Reexamination Certificate

active

06871816

ABSTRACT:
A system for automatically correcting flight path of an aircraft onto a predetermined trajectory is provided. A sensor is configured to sense speed and direction of air relative to the aircraft at a predetermined distance in front of the aircraft. A navigation system is configured to determine displacement of a flight path of the aircraft from a predetermined trajectory. A processor is coupled to receive the sensed speed and direction of air from the sensor and the displacement of the flight path from the navigation system. The processor includes a first component that is configured to determine whether the speed of the air at the predetermined distance is indicative of turbulence, and a second component that is configured to automatically generate control signals to correct the flight path of the aircraft from the displacement onto the predetermined trajectory by a time when the aircraft enters the turbulence.

REFERENCES:
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patent: 4266130 (1981-05-01), Kuhn
patent: 4342912 (1982-08-01), Adamson
patent: 4359640 (1982-11-01), Geiger
patent: 4427306 (1984-01-01), Adamson
patent: 5272513 (1993-12-01), Vahala et al.
patent: 6343766 (2002-02-01), Livingston

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