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The Application of Some Nonlinear Techniques for the Improvement of Aircraft Beam Following
Author(s): Markusen, David L., Norton, John S., Pomeroy, Orville P.
Corporate Author(s): Honeywell, Inc.
Date of Publication: 1953-02
Report number: WADC TR 53-74
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Advanced Flight Vehicle Self-Adaptive Flight Control System. Part I. Study
Author(s): Boskovich, Boris, Cole, George H., Mellen, David
Corporate Author(s): Honeywell, Inc.
Date of Publication: 1960-09
Report number: WADD TR 60-651 Part 1
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Advanced Flight Vehicle Self-Adaptive Flight Control System. Part VI. Final Flight Test Report
Author(s): Lidahl, J., McGuire, W., Reed, M.
Corporate Author(s): Honeywell, Inc.
Date of Publication: 1963-10
Report number: WADD TR 60-651 Part 6
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Advanced Flight Vehicle Adaptive Flight Control System. Part VII. Final Report on Study, Development, and Test of the MH-96 System for the X-15
Author(s): Lidahl, J., McGuire, W., Reed, M.
Corporate Author(s): Honeywell, Inc.
Date of Publication: 1963-12
Report number: WADD TR 60-651 Part 7
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Re-Entry Vehicle Control System Design and Mechanization
Author(s): Scharmack, D. K., Ward, M. D.
Corporate Author(s): Honeywell, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-04
Report number: AFFDL TR 66-3
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A Design Procedure and Handling-Quality Criteria for Lateral-Directional Flight Control Systems
Author(s): Stein, Gunter, Henke, Allen H.
Corporate Author(s): Honeywell, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1971-05
Report number: AFFDL TR 70-152
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Investigation of the Effects of Gusts on V/STOL Craft in Transition and Hover
Author(s): Skelton, Grant B.
Corporate Author(s): Honeywell, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1968-10
Report number: AFFDL TR 68-85
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Design Method for Fully Augmented Systems for Variable Flight Conditions
Author(s): VanDierendonck, Albert J.
Corporate Author(s): Honeywell, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1972-01
Report number: AFFDL-TR-71-152

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