A Flight Dynamics Evaluation of a Singer-Link GAT-2 as a Quasi-Simulator with Control Modifications.
ILLINOIS UNIV SAVOY AVIATION RESEARCH LAB
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The flight dynamics of a Singer-Link General Aviation Trainer-2 GAT-2 are analyzed theoretically and experimentally to determine the fidelity of the simulation of a light twin-engine airplane. The simulation is shown to be reasonable for experimental purposes. Four control modifications, sideslip compensation, lift compensation, position-position roll correspondence, and follow-up trim, are presented and documented. Author
- Test Facilities, Equipment and Methods