Control feel system, adjustable in flight, provided control feel as function of any combination of stick deflection, stick rate, aircraft normal acceleration, pitching acceleration, and pitching velocity; dynamic effects of using varied feel sources in various ratios were measured and/or calculated; frequency response plots illustrate dynamic effects of feel from several sources and combinations thereof.
Effects of control-feel configuration on airplane longitudinal control response
NASA -- Tech Note
1961
33 pages
Report
English
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Longitudinal control feel system for in-flight research on response feel
Engineering Index Backfile | 1961
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