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Study To Determine An Automatic Flight Control Configuration To Provide A Stability Augmentation Capability For High Performance Supersonic Aircraft
Author(s): Van Meter, J. T., McLane, R. C.Corporate Author(s): Minneapolis-Honeywell Regulator Company
Laboratory: Flight Control Laboratory
Date of Publication: 1957-06
Report number: WADC TR 57-349
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Honeywell's History and Philosophy in the Adaptive Control Field
Author(s): Schuck, O. HugoCorporate Author(s): Minneapolis-Honeywell Regulator Company
Laboratory: Flight Control Laboratory
Date of Publication: 1961-03
Report number: WADC TR 59-49 p. 123-145
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A Technique for Analyzing an Adaptive Flight Control System Containing a Bi-Stable Element
Author(s): Prince, Luther T.Corporate Author(s): Minneapolis-Honeywell Regulator Company
Laboratory: Flight Control Laboratory
Date of Publication: 1961-03
Report number: WADC TR 59-49 p. 148-170
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Study and Development of an Electric Side Stick Controller for Aerospace Vehicles
Author(s): Graves, Harry C., Bailey, A. James, Mellen, David L.Corporate Author(s): Minneapolis-Honeywell Regulator Company
Laboratory: Flight Control Laboratory
Date of Publication: 1962-05
Report number: ASD TR 61-603
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Control System Redundancy Mechanization Study
Author(s): Tesch, E., Plaisted, R., Pukite, J.Corporate Author(s): Minneapolis-Honeywell Regulator Company
Laboratory: Flight Control Laboratory
Date of Publication: 1963-02
Report number: ASD TDR 62-772
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