论文信息 - PILOT-INDUCED OSCILLATIONS: THEIR CAUSE AND ANALYSIS

PILOT-INDUCED OSCILLATIONS: THEIR CAUSE AND ANALYSIS

Abstract : Systems analysis techniques are applied to the problem of pilot- induced aircraft oscillations (PIO). Mathematical models used for the pilot prior to and during PIO, as well as the use of various pilot and subsystem describing functions, are reviewed. Several examples of PIO causes, analyses, and cures are given, including linear and nonlinear longitudinal PIO. The closed-loop describing function for a rate-limited position servo is derived.

[1] L Stark,et al. Dynamic Characteristics of the Motor Coordination System in Man. , 1961, Biophysical journal.

[2] Norman M Mcfadden,et al. A flight study of longitudinal-control-system dynamic characteristics by the use of a variable-control-system airplane , 1957 .

[3] Gene J. Matranga. Analysis of X-15 Landing Approach and Flare Characteristics Determined from the First 30 Flights , 1961 .

[4] Lawrence W. Taylor. Analysis of a Pilot Airplane Lateral Instability Experienced with the X-15 Airplane , 1961 .

[5] Ezra S. Krendel,et al. A servomechanisms approach to skill development , 1960 .

[6] James L. Decker,et al. The Human Pilot and the High-Speed Airplane , 1956 .

[7] Gene J. Matranga,et al. Launch, Low-Speed, and Landing Characteristics Determined from the First Flight of the North American X-15 Research Airplane , 1959 .

[8] Robert Mayne,et al. Some engineering aspects of the mechanism of body control , 1951, Electrical Engineering.

[9] W. H. Terrill,et al. Investigation of Pilot-Induced Longitudinal Oscillation in the Douglas Model A4D-2 Airplane, , 1957 .

[10] Duane T. McRuer,et al. A SYSTEMS ANALYSIS VIEW OF LONGITUDINAL FLYING QUALITIES , 1960 .