Pitch Controllability Based on Airplane Model without Short-Period Approximation—Flight Simulator Experiment—

Author:

Sato Osamu,Kobayashi Osamu

Publisher

Japan Society for Aeronautical and Space Sciences

Reference10 articles.

1. Simulator investigation of the effects of l alpha and true speed on longitudinal handling qualities

2. 2) Etkin, B.: Dynamics of Atmospheric Flight, John Wiley & Sons, Inc., New York, 1972, pp. 501–518.

3. 3) Anon: Military Specification, Flying Qualities of Piloted Airplanes, MIL-F-8785C, 1980.

4. 4) Chalk, C. R., Neal, T. P., Harris, F. E., Pritchard, F. E. and Woodcock, R. J.: Background Information and User Guide for MIL-F-8785B (ASG), Military Specification—Flying Qualities of Piloted Airplanes, Air Force Flight Dynamics Laboratory, AFFDL-TR-69-72, 1969.

5. 5) Grantham, W. D., Nguyen, L. T., Patton, J. M., Deal, P. L. and Champine, R. A.: Fixed-Base Simulator Study of an Externally Blown Flap STOL Transport Airplane during Approach and Landing, NASA-TN-D-6898, 1972.

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