Simulating horizontal stabilizer trimming in an aircraft
Number of patents in Portfolio can not be more than 2000
United States of America Patent
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-
Feb 15, 1994
Grant Date -
N/A
app pub date -
Oct 7, 1992
filing date -
Oct 7, 1992
priority date (Note) -
Expired
status (Latency Note)
Importance
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.
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