Simulating horizontal stabilizer trimming in an aircraft

Education and demonstration – Vehicle operator instruction or testing – Flight vehicle

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244178, G09B 900

Patent

active

052862038

ABSTRACT:
The present invention features a simulator apparatus and method for realistically simulating actual forces at the horizontal stabilizer trim controls of an aircraft. The invention features a closed-loop, microprocessor-based programmable system with reduced mechanical, electromechanical, and/or hydraulic components. The microprocessor computes the required reaction forces using a softward model of the horizontal stabilizer trim system.

REFERENCES:
patent: 4504233 (1985-03-01), Galus et al.
patent: 4599070 (1985-07-01), Hladky et al.
patent: 4710128 (1987-12-01), Wachsmuth et al.
patent: 4751662 (1988-06-01), Croshie
patent: 4820162 (1989-04-01), Ross
patent: 5009598 (1991-04-01), Bennington
patent: 5158459 (1992-10-01), Edelberg

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