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Flying Qualities Research Using an In-Flight Simulator
ISSN: 0148-7191, e-ISSN: 2688-3627
Published February 01, 1967 by SAE International in United States
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The variable-stability airplane used as in in-flight simulator has been an important and effective research tool in the field of handling qualities requirements for military aircraft. Such a machine is equally well-suited for studies of the general aviation airplane-pilot combination, with the objective of defining optimum and minimum acceptable values of flying qualities parameters for use as design and certification guides.
CitationEllis, D. and Miller, G., "Flying Qualities Research Using an In-Flight Simulator," SAE Technical Paper 670261, 1967, https://doi.org/10.4271/670261.
- Seckel, E. Miller, G. E. and Nixon, W. B. “Lateral-Directional Flying Qualities for Power Approach.” Princeton University Report No. 727, September 1966.
- Eney, J. A. “Comparative Flight Evaluation of Longitudinal Handling Qualities in Carrier Approach.” Princeton University Report No. 777, May 1966.