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.
Type:
Grant
Filed:
October 7, 1992
Date of Patent:
February 15, 1994
Assignee:
AAI Microflite Simulation International
Inventors:
John J. Fuller, Charles J. Bratt, Wayne Blackwell, Paul E. Mueller