A procedure for estimating stability and control parameters from flight test data by using maximum likelihood methods employing a real-time digital system /

Piloted simulation of an algorithm for onboard control of time-optimal intercept /

Price, Douglas B. (Douglas Bailey), 1942-
Moerder, Daniel D.
Calise, Anthony J.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 44).M...

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

Flight-determined derivatives and dynamic characteristics of the CV-990 airplane /

Gilyard, Glenn B.
Flight Research Center (U.S.)

January 1972

Prepared at NASA Flight Research Center.Cover title.Bibliography: p. 24.Mode of access: Internet

Maximum likelihood method for estimating airplane stability and control parameters from flight data in frequency domain /

Klein, Vladislav.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

Subject Category 08."May 1980"--Cover."Langley Research Center."Includes bibliographical references....

Practical aspects of using a maximum likelihood estimation method to extract stability and control derivitives from flight data /

Iliff, Kenneth W.
Maine, Richard E., joint author.
United States. National Aeronautics and Space Administration.
Hugh L. Dryden Flight Research Center.

January 1976

Cover title.Includes bibliographical references (p. 32).Mode of access: Internet

Maximum likelihood identification and optimal input design for identifying aircraft stability and control derivatives /

Stepner, David E.
Mehra, Raman K.
Langley Research Center.
Systems Control, inc.

January 1973

"Prepared by Systems Control ... for Langley Research Center."Cover title.Includes bibliographical r...

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

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

A FORTRAN program for determining aircraft stability and control derivatives from flight data /

Maine, Richard E.
Iliff, Kenneth W.
Flight Research Center (U.S.)

January 1975

Prepared at the NASA Flight Research Center.Cover title.Includes bibliographical references (p. 171)...

Flight testing techniques for the evaluation of light aircraft stability derivitives : a review and analysis /

Smetana, Frederick O.
Johnson, W. Donald.
Summey, Delbert C.
Langley Research Center.
United States. National Aeronautics and Space Administration.
North Carolina State University.

January 1972

N72-24991."Prepared by North Carolina State University ... for Langley Research Center."Cover title....

Analysis of flight data from a high-incidence research model by system identification methods /

Batterson, James G.
Klein, Vladislav.
Langley Research Center.

January 1989

Research performed at Langley Research Center.Bibliography: p. 12.Mode of access: Internet

Estimation of airplane stability and control derivatives from large amplitude longitudinal maneuvers /

Batterson, James G.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject Category 08."October 1981"--Cover."Langley Research Center."Bibliography: p. 18.Mode of acce...

Flight control system design factors for applying automated testing techniques /

Sitz, Joel R.
Vernon, Todd H.
Dryden Flight Research Facility.

January 1990

Prepared at Dryden Flight Research Facility, Ames Research Center.Bibliography: p. 7-8.Mode of acces...

Procedure for estimating stability and control parameters from flight test data by using maximum likelihood methods employing a real-time digital system

Grove, R. D.
Mayhew, S. C.
Bowles, R. L.

May 1972

A maximum likelihood parameter estimation procedure and program were developed for the extraction of...

Longitudinal stability and control derivatives of a jet fighter airplane extracted from flight test data by utilizing maximum likelihood estimation /

Steinmetz, George G.
Parrish, Russell V.
Bowles, Roland L.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1972

"A method of parameter extraction for stability and control derivatives of aircraft from flight test...

Piloted simulation of an algorithm for onboard control of time-optimal intercept /

Price, Douglas B. (Douglas Bailey), 1942-
Moerder, Daniel D.
Calise, Anthony J.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 44).M...

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

Flight-determined derivatives and dynamic characteristics of the CV-990 airplane /

Gilyard, Glenn B.
Flight Research Center (U.S.)

January 1972

Prepared at NASA Flight Research Center.Cover title.Bibliography: p. 24.Mode of access: Internet

Maximum likelihood method for estimating airplane stability and control parameters from flight data in frequency domain /

Klein, Vladislav.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

Subject Category 08."May 1980"--Cover."Langley Research Center."Includes bibliographical references....

Practical aspects of using a maximum likelihood estimation method to extract stability and control derivitives from flight data /

Iliff, Kenneth W.
Maine, Richard E., joint author.
United States. National Aeronautics and Space Administration.
Hugh L. Dryden Flight Research Center.

January 1976

Cover title.Includes bibliographical references (p. 32).Mode of access: Internet

Maximum likelihood identification and optimal input design for identifying aircraft stability and control derivatives /

Stepner, David E.
Mehra, Raman K.
Langley Research Center.
Systems Control, inc.

January 1973

"Prepared by Systems Control ... for Langley Research Center."Cover title.Includes bibliographical r...

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

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

A FORTRAN program for determining aircraft stability and control derivatives from flight data /

Maine, Richard E.
Iliff, Kenneth W.
Flight Research Center (U.S.)

January 1975

Prepared at the NASA Flight Research Center.Cover title.Includes bibliographical references (p. 171)...

Flight testing techniques for the evaluation of light aircraft stability derivitives : a review and analysis /

Smetana, Frederick O.
Johnson, W. Donald.
Summey, Delbert C.
Langley Research Center.
United States. National Aeronautics and Space Administration.
North Carolina State University.

January 1972

N72-24991."Prepared by North Carolina State University ... for Langley Research Center."Cover title....

Analysis of flight data from a high-incidence research model by system identification methods /

Batterson, James G.
Klein, Vladislav.
Langley Research Center.

January 1989

Research performed at Langley Research Center.Bibliography: p. 12.Mode of access: Internet

Estimation of airplane stability and control derivatives from large amplitude longitudinal maneuvers /

Batterson, James G.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject Category 08."October 1981"--Cover."Langley Research Center."Bibliography: p. 18.Mode of acce...

Flight control system design factors for applying automated testing techniques /

Sitz, Joel R.
Vernon, Todd H.
Dryden Flight Research Facility.

January 1990

Prepared at Dryden Flight Research Facility, Ames Research Center.Bibliography: p. 7-8.Mode of acces...

Procedure for estimating stability and control parameters from flight test data by using maximum likelihood methods employing a real-time digital system

Grove, R. D.
Mayhew, S. C.
Bowles, R. L.

May 1972

A maximum likelihood parameter estimation procedure and program were developed for the extraction of...

Longitudinal stability and control derivatives of a jet fighter airplane extracted from flight test data by utilizing maximum likelihood estimation /

Steinmetz, George G.
Parrish, Russell V.
Bowles, Roland L.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1972

"A method of parameter extraction for stability and control derivatives of aircraft from flight test...

Piloted simulation of an algorithm for onboard control of time-optimal intercept /

Price, Douglas B. (Douglas Bailey), 1942-
Moerder, Daniel D.
Calise, Anthony J.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 44).M...

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

Flight-determined derivatives and dynamic characteristics of the CV-990 airplane /

Gilyard, Glenn B.
Flight Research Center (U.S.)

January 1972

Prepared at NASA Flight Research Center.Cover title.Bibliography: p. 24.Mode of access: Internet

A procedure for estimating stability and control parameters from flight test data by using maximum likelihood methods employing a real-time digital system /

Abstract

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A procedure for estimating stability and control parameters from flight test data by using maximum likelihood methods employing a real-time digital system /

Abstract

Extracted data

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