Reduced order feedback control equations for linear time and frequency domain analysis /

Modeling digital control systems with MA-prefiltered measurements /

Polites, Michael E. (Michael Edward)
George C. Marshall Space Flight Center. Structures and Dynamics Laboratory.

January 1987

Prepared at the Structures and Dynamics Laboratory, George C. Marshall Space Flight Center."June 198...

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...

Optimum nonlinear control of a second order nonlinear system /

Oldenburger, Rufus, 1908-
Gamble, E. H.
Nicklas, John C.
Purdue University.

Prepared at Purdue University."April 1961."Cover title.Includes bibliographical references (p. 50-54...

Time and frequency domain analysis of sampled data controllers via mixed operation equations /

Frisch, Harold P.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Goddard Space Flight Center.

January 1981

"June 1981--Cover."Goddard Space Flight Center."Includes bibliographical references.Mode of access: ...

A Method for obtaining reduced-order control laws for high-order systems using optimization techniques /

Mukhopadhyay, Vivek.
Abel, Irving.
Newsom, Jerry R.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"August 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: I...

The analysis and design of continuous and sampled-data feedback control systems with a saturation type nonlinearity /

Schmidt, Stanley Francis.
Ames Research Center.

January 1959

"NASA TN D-20.""Ames Research Center, Moffett Field, Calif.""August 1959."Cover title.Mode of access...

Pitfalls and guidelines for the numerical evaluation of moderate-order system frequency response /

Frisch, Harold P.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Goddard Space Flight Center.

January 1981

"June 1981--Cover."Goddard Space Flight Center."Bibliography: p. 27-29.Mode of access: Internet

A method for obtaining practical flutter-suppression control laws using results of optimal control theory /

Newsom, Jerry R.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"August 1979"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: I...

Application of model control to wing-flutter suppression /

Ostroff, Aaron J.
Pines, Samuel.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

"May 1982"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: Inte...

The design of feedback control systems containing a saturation type nonlinearity. /

Schmidt, Stanley F.
Harper, Eleanor V.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Aircraft; Stability and control.Includes bibliographical references.Mod...

Stability boundaries for systems with frequency-model feedback and complementary filter /

Barker, L. Keith.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Nov. 1980."Langley Research Center."Includes bibliographical references.Mode of access: Internet

Investigation, development, and application of optimal output feedback theory.

Broussard, John R.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1987

"Prepared for Langley Research Center under Contract NAS1-15759.""December 1987."Cover title.Include...

Optimal pseudo-derivative-feedback control/

Ulsoy, Ali Galip, 1950-

January 1975

Thesis (M.S.)--Cornell University, Jan., 1975.Bibliography: leaves 56-57.Mode of access: Internet

A transient response method for linear coupled substructures /

Admire, J. R.
Brunty, J. A.
George C. Marshall Space Flight Center.

January 1989

Prepared at George C. Marshall Space Flight Center.Bibliography: p. 19-20.Mode of access: Internet

Resonance-inert stabilization for space stations /

Von Pragenau, G. L.
George C. Marshall Space Flight Center.

January 1972

Prepared at George C. Marshall Space Flight Center.Cover title.Bibliography: p. 33-35.Mode of access...

Modeling digital control systems with MA-prefiltered measurements /

Polites, Michael E. (Michael Edward)
George C. Marshall Space Flight Center. Structures and Dynamics Laboratory.

January 1987

Prepared at the Structures and Dynamics Laboratory, George C. Marshall Space Flight Center."June 198...

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...

Optimum nonlinear control of a second order nonlinear system /

Oldenburger, Rufus, 1908-
Gamble, E. H.
Nicklas, John C.
Purdue University.

Prepared at Purdue University."April 1961."Cover title.Includes bibliographical references (p. 50-54...

Time and frequency domain analysis of sampled data controllers via mixed operation equations /

Frisch, Harold P.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Goddard Space Flight Center.

January 1981

"June 1981--Cover."Goddard Space Flight Center."Includes bibliographical references.Mode of access: ...

A Method for obtaining reduced-order control laws for high-order systems using optimization techniques /

Mukhopadhyay, Vivek.
Abel, Irving.
Newsom, Jerry R.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"August 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: I...

The analysis and design of continuous and sampled-data feedback control systems with a saturation type nonlinearity /

Schmidt, Stanley Francis.
Ames Research Center.

January 1959

"NASA TN D-20.""Ames Research Center, Moffett Field, Calif.""August 1959."Cover title.Mode of access...

Pitfalls and guidelines for the numerical evaluation of moderate-order system frequency response /

Frisch, Harold P.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Goddard Space Flight Center.

January 1981

"June 1981--Cover."Goddard Space Flight Center."Bibliography: p. 27-29.Mode of access: Internet

A method for obtaining practical flutter-suppression control laws using results of optimal control theory /

Newsom, Jerry R.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"August 1979"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: I...

Application of model control to wing-flutter suppression /

Ostroff, Aaron J.
Pines, Samuel.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

"May 1982"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: Inte...

The design of feedback control systems containing a saturation type nonlinearity. /

Schmidt, Stanley F.
Harper, Eleanor V.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Aircraft; Stability and control.Includes bibliographical references.Mod...

Stability boundaries for systems with frequency-model feedback and complementary filter /

Barker, L. Keith.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Nov. 1980."Langley Research Center."Includes bibliographical references.Mode of access: Internet

Investigation, development, and application of optimal output feedback theory.

Broussard, John R.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1987

"Prepared for Langley Research Center under Contract NAS1-15759.""December 1987."Cover title.Include...

Optimal pseudo-derivative-feedback control/

Ulsoy, Ali Galip, 1950-

January 1975

Thesis (M.S.)--Cornell University, Jan., 1975.Bibliography: leaves 56-57.Mode of access: Internet

A transient response method for linear coupled substructures /

Admire, J. R.
Brunty, J. A.
George C. Marshall Space Flight Center.

January 1989

Prepared at George C. Marshall Space Flight Center.Bibliography: p. 19-20.Mode of access: Internet

Resonance-inert stabilization for space stations /

Von Pragenau, G. L.
George C. Marshall Space Flight Center.

January 1972

Prepared at George C. Marshall Space Flight Center.Cover title.Bibliography: p. 33-35.Mode of access...

Modeling digital control systems with MA-prefiltered measurements /

Polites, Michael E. (Michael Edward)
George C. Marshall Space Flight Center. Structures and Dynamics Laboratory.

January 1987

Prepared at the Structures and Dynamics Laboratory, George C. Marshall Space Flight Center."June 198...

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...

Optimum nonlinear control of a second order nonlinear system /

Oldenburger, Rufus, 1908-
Gamble, E. H.
Nicklas, John C.
Purdue University.

Prepared at Purdue University."April 1961."Cover title.Includes bibliographical references (p. 50-54...

Reduced order feedback control equations for linear time and frequency domain analysis /

Abstract

Extracted data

Reduced order feedback control equations for linear time and frequency domain analysis /

Abstract

Extracted data

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