New tentative criteria have been developed for airplanes with relaxed static longitudinal stability based on approach and landing ground simulation, but augmented by the available flight test data. It is shown that a criterion based on just time-to-double amplitude is invalid, and other elements in the pitch attitude transfer function must be included. Criteria based on both closed-loop frequency response and airplane parameters (open-loop) are developed. This report covers the results obtained in one of a series of Air Force programs to update MIL-F-8785, 'Flying Qualities of Piloted Airplanes'.
Proposed Revisions to MIL-F-8785C Related to Flight Safety of Augmented Aircraft. Volume 3. Appendix G. Pilot Comments
1982
123 pages
Report
Keine Angabe
Englisch
Avionics , Aircraft , Flight control systems , Flight maneuvers , Static stability , Pitch(Inclination) , Roll , Stalling , Approach , Aircraft landings , Closed loop systems , Frequency response , Open loop systems , Parameters , Man machine systems , Pilots , Flight crews , Interviewing , Aviation safety , Handling , Military aircraft , Augmentation , Specifications , User manuals , Handbooks , Flying qualities , Longitudinal flying qualities , Relaxed static stability , Pilot comments , Attitude
Invitation for Comments on Proposed Revisions to ITE Policies
Online Contents | 1993
GENERAL DISCUSSION OF SAFETY REGULATIONS AND PROPOSED REVISIONS
SAE Technical Papers | 1959
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