Flight control system design factors for applying automated testing techniques /

Ground and flight test methods for determining limit cycle and structural resonance characteristics of aircraft stability augmentation systems /

Painter, Weneth D.
Sitterle, George J.
Flight Research Center (U.S.)

January 1972

Prepared at the NASA Flight Research Center.Cover title.Bibliography: p. 20.Mode of access: Internet

An in-flight technique for wind measurement in support of the space shuttle program /

Bjarke, Lisa J.
Ehernberger, L. J.
Dryden Flight Research Facility.

January 1989

Research performed at Dryden Flight Research Facility.Bibliography: p. 6.Mode of access: Internet

Conceptual design optimization study /

Hollowell, S. J.
Hiyama, R. M.
Beeman, E. R.
Langley Research Center.
North American Aircraft (Firm)

January 1990

Prepared at North American Aircraft, Rockwell International Corporation, for Langley Research Center...

Propulsion system/flight control integration and optimization : flight evaluation and technology transition /

Burcham, Frank W.
Myers, Lawrence P.
Gilyard, Glenn B.
Dryden Flight Research Facility.

January 1990

Prepared at Dryden Flight Research Facility.Bibliography: p. 9-10.Mode of access: Internet

A Preliminary investigation of the use of throttles for emergency flight control /

Burcham, Frank W.
Dryden Flight Research Facility.

January 1991

Prepared at Dryden Flight Research Facility.Bibliography: p. 9.Mode of access: Internet

A controls engineering approach for analyzing airplane input-output characteristics /

Arbuckle, P. Douglas (Paul Douglas)
Langley Research Center.

January 1991

Prepared at Langley Research Center.Bibliography: p. 17.Mode of access: Internet

Development of an integrated aeroservoelastic analysis program and correlation with test data /

Gupta, Kajal K.
Voelker, L. S.
Brenner, M. J.
Dryden Flight Research Facility.

January 1991

Prepared at the Dryden Flight Research Facility.Bibliography: p. 39.Mode of access: Internet

Automated procedure for design of wing structures to satisfy strength and flutter requirements /

Haftka, Raphael T.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 22-24.Mode of access: Internet

Aircraft flight test trajectory control /

Menon, P. K. A. (Padmanabhan K. A.)
Walker, R. A.
Dryden Flight Research Facility.

January 1988

"August 1988"--Cover."Prepared for Ames Research Center, Dryden Flight Research Facility under Contr...

Development and flight test results of an autothrottle control system at Mach 3 cruise /

Gilyard, Glenn B.
Burken, John J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Hugh L. Dryden Flight Research Center.

January 1980

"July 1980"--Cover.Subject category 08."Dryden Flight Research Center."Mode of access: Internet

Flight evaluation of advanced control systems and displays on a general aviation airplane /

Loschke, Paul C.
Flight Research Center (U.S.)

January 1974

Prepared at the NASA Flight Research Center.Cover title.Includes bibliographical references (p. 18)....

A knowledge based application of the extended aircraft interrogation and display system /

Glover, Richard D.
Larson, Richard R.
Dryden Flight Research Facility.

January 1991

Prepared at the Dryden Flight Research Facility.Bibliography: p. 26.Mode of access: Internet

Flight investigation of a structural mode control system for the XB-70 aircraft /

Lock, Wilton P.
Flight Research Center (U.S.)

January 1973

Prepared at NASA Flight Research Center.Cover title.Includes bibliographical references (p. 22).Mode...

Preliminary system design study for a digital fly-by-wire flight control system for an F-8C aircraft /

Seacord, C. L.
Vaughn, Darrel.
Langley Research Center.
Honeywell Inc.

"Prepared by Honeywell, Inc. ... for Langley Research Center.""January 1976."Cover title.Includes bi...

Flight investigation of manual and automatic VTOL decelerating instrument approaches and landings /

Kelly, James R.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Bibliography: p. 22.Mode of access: Internet

Ground and flight test methods for determining limit cycle and structural resonance characteristics of aircraft stability augmentation systems /

Painter, Weneth D.
Sitterle, George J.
Flight Research Center (U.S.)

January 1972

Prepared at the NASA Flight Research Center.Cover title.Bibliography: p. 20.Mode of access: Internet

An in-flight technique for wind measurement in support of the space shuttle program /

Bjarke, Lisa J.
Ehernberger, L. J.
Dryden Flight Research Facility.

January 1989

Research performed at Dryden Flight Research Facility.Bibliography: p. 6.Mode of access: Internet

Conceptual design optimization study /

Hollowell, S. J.
Hiyama, R. M.
Beeman, E. R.
Langley Research Center.
North American Aircraft (Firm)

January 1990

Prepared at North American Aircraft, Rockwell International Corporation, for Langley Research Center...

Propulsion system/flight control integration and optimization : flight evaluation and technology transition /

Burcham, Frank W.
Myers, Lawrence P.
Gilyard, Glenn B.
Dryden Flight Research Facility.

January 1990

Prepared at Dryden Flight Research Facility.Bibliography: p. 9-10.Mode of access: Internet

A Preliminary investigation of the use of throttles for emergency flight control /

Burcham, Frank W.
Dryden Flight Research Facility.

January 1991

Prepared at Dryden Flight Research Facility.Bibliography: p. 9.Mode of access: Internet

A controls engineering approach for analyzing airplane input-output characteristics /

Arbuckle, P. Douglas (Paul Douglas)
Langley Research Center.

January 1991

Prepared at Langley Research Center.Bibliography: p. 17.Mode of access: Internet

Development of an integrated aeroservoelastic analysis program and correlation with test data /

Gupta, Kajal K.
Voelker, L. S.
Brenner, M. J.
Dryden Flight Research Facility.

January 1991

Prepared at the Dryden Flight Research Facility.Bibliography: p. 39.Mode of access: Internet

Automated procedure for design of wing structures to satisfy strength and flutter requirements /

Haftka, Raphael T.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 22-24.Mode of access: Internet

Aircraft flight test trajectory control /

Menon, P. K. A. (Padmanabhan K. A.)
Walker, R. A.
Dryden Flight Research Facility.

January 1988

"August 1988"--Cover."Prepared for Ames Research Center, Dryden Flight Research Facility under Contr...

Development and flight test results of an autothrottle control system at Mach 3 cruise /

Gilyard, Glenn B.
Burken, John J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Hugh L. Dryden Flight Research Center.

January 1980

"July 1980"--Cover.Subject category 08."Dryden Flight Research Center."Mode of access: Internet

Flight evaluation of advanced control systems and displays on a general aviation airplane /

Loschke, Paul C.
Flight Research Center (U.S.)

January 1974

Prepared at the NASA Flight Research Center.Cover title.Includes bibliographical references (p. 18)....

A knowledge based application of the extended aircraft interrogation and display system /

Glover, Richard D.
Larson, Richard R.
Dryden Flight Research Facility.

January 1991

Prepared at the Dryden Flight Research Facility.Bibliography: p. 26.Mode of access: Internet

Flight investigation of a structural mode control system for the XB-70 aircraft /

Lock, Wilton P.
Flight Research Center (U.S.)

January 1973

Prepared at NASA Flight Research Center.Cover title.Includes bibliographical references (p. 22).Mode...

Preliminary system design study for a digital fly-by-wire flight control system for an F-8C aircraft /

Seacord, C. L.
Vaughn, Darrel.
Langley Research Center.
Honeywell Inc.

"Prepared by Honeywell, Inc. ... for Langley Research Center.""January 1976."Cover title.Includes bi...

Flight investigation of manual and automatic VTOL decelerating instrument approaches and landings /

Kelly, James R.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Bibliography: p. 22.Mode of access: Internet

Ground and flight test methods for determining limit cycle and structural resonance characteristics of aircraft stability augmentation systems /

Painter, Weneth D.
Sitterle, George J.
Flight Research Center (U.S.)

January 1972

Prepared at the NASA Flight Research Center.Cover title.Bibliography: p. 20.Mode of access: Internet

An in-flight technique for wind measurement in support of the space shuttle program /

Bjarke, Lisa J.
Ehernberger, L. J.
Dryden Flight Research Facility.

January 1989

Research performed at Dryden Flight Research Facility.Bibliography: p. 6.Mode of access: Internet

Conceptual design optimization study /

Hollowell, S. J.
Hiyama, R. M.
Beeman, E. R.
Langley Research Center.
North American Aircraft (Firm)

January 1990

Prepared at North American Aircraft, Rockwell International Corporation, for Langley Research Center...

Flight control system design factors for applying automated testing techniques /

Abstract

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Flight control system design factors for applying automated testing techniques /

Abstract

Extracted data

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