Patents Assigned to AAI Microflite Simulation International
  • Patent number: 5286203
    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