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

Research in digital adaptive flight controllers /

Kaufman, Howard.
United States. National Aeronautics and Space Administration.
Langley Research Center.
Rensselaer Polytechnic Institute.

January 1976

Cover title.Includes bibliographical references (p. 85-87).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

Analog-computer investigation of effects of friction and preload on the dynamic longitudinal characteristics of a pilot-airplane combination. /

Crane, Harold L.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aircraft; Simulators and computers; Stability and control.Includes bibliograp...

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)....

Input design for identification of aircraft stability and control derivatives /

Gupta, Narendra K. (Narendra Kumar)
Hall, W. Earl.
Flight Research Center (U.S.)
Systems Control, inc.

"Prepared by Systems Control, Inc. ... for Flight Research Center.""February 1975."Cover title.Inclu...

Effects of time-shifted data on flight-determined stability and control derivatives /

Steers, Sandra Thornberry.
Iliff, Kenneth W.
Flight Research Center (U.S.)

January 1975

Prepared at the NASA Flight Research Center.Cover title.Includes bibliographical references (p. 11)....

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...

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

Grove, Randall D.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 44-45.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

FORTRAN program for induction motor analysis /

Bollenbacher, Gary.
Lewis Research Center.

January 1976

Cover title.Includes bibliographical references (p. 70).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...

FORTRAN program for predicting off-design performance of centrifugal compressors /

Galvas, Michael R.
U.S. Army Air Mobility Research and Development Laboratory.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center and the U.S. Army Air Mobility R&D Laboratory.Cover title.Includes...

Flutter analysis of swept-wing subsonic aircraft with parameter studies of composite wings /

Housner, Jerrold M.
Stein, Manuel.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 93).Mode of ...

Numerical methods for the design and analysis of wings at supersonic speeds /

Carlson, Harry W.
Miller, David S.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 29-30).Mode ...

Stability analysis for laminar flow control.

Benney, David J.
Orszag, Steven A.
Langley Research Center.
Cambridge Hydrodynamics, inc.

Pt. II issued by NASA's Scientific and Technical Information Office.Cover title--pt. I.Includes bibl...

Research in digital adaptive flight controllers /

Kaufman, Howard.
United States. National Aeronautics and Space Administration.
Langley Research Center.
Rensselaer Polytechnic Institute.

January 1976

Cover title.Includes bibliographical references (p. 85-87).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

Analog-computer investigation of effects of friction and preload on the dynamic longitudinal characteristics of a pilot-airplane combination. /

Crane, Harold L.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aircraft; Simulators and computers; Stability and control.Includes bibliograp...

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)....

Input design for identification of aircraft stability and control derivatives /

Gupta, Narendra K. (Narendra Kumar)
Hall, W. Earl.
Flight Research Center (U.S.)
Systems Control, inc.

"Prepared by Systems Control, Inc. ... for Flight Research Center.""February 1975."Cover title.Inclu...

Effects of time-shifted data on flight-determined stability and control derivatives /

Steers, Sandra Thornberry.
Iliff, Kenneth W.
Flight Research Center (U.S.)

January 1975

Prepared at the NASA Flight Research Center.Cover title.Includes bibliographical references (p. 11)....

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...

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

Grove, Randall D.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 44-45.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

FORTRAN program for induction motor analysis /

Bollenbacher, Gary.
Lewis Research Center.

January 1976

Cover title.Includes bibliographical references (p. 70).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...

FORTRAN program for predicting off-design performance of centrifugal compressors /

Galvas, Michael R.
U.S. Army Air Mobility Research and Development Laboratory.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center and the U.S. Army Air Mobility R&D Laboratory.Cover title.Includes...

Flutter analysis of swept-wing subsonic aircraft with parameter studies of composite wings /

Housner, Jerrold M.
Stein, Manuel.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 93).Mode of ...

Numerical methods for the design and analysis of wings at supersonic speeds /

Carlson, Harry W.
Miller, David S.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 29-30).Mode ...

Stability analysis for laminar flow control.

Benney, David J.
Orszag, Steven A.
Langley Research Center.
Cambridge Hydrodynamics, inc.

Pt. II issued by NASA's Scientific and Technical Information Office.Cover title--pt. I.Includes bibl...

Research in digital adaptive flight controllers /

Kaufman, Howard.
United States. National Aeronautics and Space Administration.
Langley Research Center.
Rensselaer Polytechnic Institute.

January 1976

Cover title.Includes bibliographical references (p. 85-87).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

Analog-computer investigation of effects of friction and preload on the dynamic longitudinal characteristics of a pilot-airplane combination. /

Crane, Harold L.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aircraft; Simulators and computers; Stability and control.Includes bibliograp...

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

Abstract

Extracted data

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

Abstract

Extracted data

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