Classical eighth- and lower-order Runge-Kutta-Nyström formulas with a new stepsize control procedure for special second-order differential equations /

Low thrust space vehicle trajectory optimization using regularized variables /

Schwenzfeger, K. J.
George C. Marshall Space Flight Center.

January 1974

Prepared at George C. Marshall Space Flight Center.Cover title.Includes bibliographical references (...

Numerical integration in a rigid-body trajectory program /

Moore, John Edd.
United States. National Aeronautics and Space Administration.
Aero-Astrodynamics Laboratory (George C. Marshall Space Flight Center)

Comparison of fourth order Runge-Kutta numerical integration technique with two numerical integratio...

The computation of partial volumes of the components in solution /

Rosen, Joseph S. (Joseph Selwyn)
George C. Marshall Space Flight Center.

Prepared at George C. Marshall Space Flight Center."December 1967"--Cover.Includes bibliographical r...

Classical seventh-, sixth-, and fifth-order Runge-Kutta-Nyström formulas with stepsize control for general second-order differential equations /

Fehlberg, Erwin.
George C. Marshall Space Flight Center.

January 1974

Prepared at Marshall Space Flight Center.Cover title.Includes bibliographical references (p. 41).Mod...

The Runge-Kutta equations by quadrature methods /

Rosen, Joseph S.
George C. Marshall Space Flight Center.

January 1967

"November 1967."Includes bibliographical references.Performed by George C. Marshall Space Flight Cen...

Approximate solutions of Runge-Kutta equations /

Rosen, Joseph S.
United States. National Aeronautics and Space Administration.
George C. Marshall Space Flight Center.

January 1967

Prepared at George C. Marshall Space Flight Center."August 1967"--Cover.Includes bibliographical ref...

Numerical solution of differential equations using Obrechkoff corrector formulas /

Rosen, Joseph S. (Joseph Selwyn)
United States. National Aeronautics and Space Administration.
George C. Marshall Space Flight Center.

Solution of differential equations by predictor corrector formulas for high order accuracy.Prepared ...

Numerically stable interpolation formulas with favorable error propagation for first- and second-order differential equations /

Fehlberg, Erwin.
George C. Marshall Space Flight Center.

Prepared at George C. Marshall Space Flight Center."March 1961."Cover title.Includes bibliographical...

Classical Fifth-, Sixth-, Seventh-, and Eighth-Order Runge-Kutta Formulas with Stepsize Control

Fehlberg, E.

October 1968

Runge-Kutta formulas of high order with stepsize control through leading truncation error ter

Development of a general formula expanding the higher-order derivatives of the function tanh z in powers of tanh z and A-numbers /

Hosenthien, Hans H.

Prepared at George C. Marshall Space Flight Center."January 1968"--Cover.Includes bibliographical re...

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...

Second-order small-disturbance solutions for hypersonic flow over power-law bodies /

Townsend, James C. (James Courtland), 1938-
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 57-58).Mode ...

On the error propagation of some interpolation formulas for second-order differential equations : by Erwin Fehlberg.

Fehlberg, Erwin.
George C. Marshall Space Flight Center.

Prepared at George C. Marshall Space Flight Center."July 1963"--Cover.Includes bibliographical refer...

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

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. 21-22.Mode of access: Internet

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...

Low thrust space vehicle trajectory optimization using regularized variables /

Schwenzfeger, K. J.
George C. Marshall Space Flight Center.

January 1974

Prepared at George C. Marshall Space Flight Center.Cover title.Includes bibliographical references (...

Numerical integration in a rigid-body trajectory program /

Moore, John Edd.
United States. National Aeronautics and Space Administration.
Aero-Astrodynamics Laboratory (George C. Marshall Space Flight Center)

Comparison of fourth order Runge-Kutta numerical integration technique with two numerical integratio...

The computation of partial volumes of the components in solution /

Rosen, Joseph S. (Joseph Selwyn)
George C. Marshall Space Flight Center.

Prepared at George C. Marshall Space Flight Center."December 1967"--Cover.Includes bibliographical r...

Classical seventh-, sixth-, and fifth-order Runge-Kutta-Nyström formulas with stepsize control for general second-order differential equations /

Fehlberg, Erwin.
George C. Marshall Space Flight Center.

January 1974

Prepared at Marshall Space Flight Center.Cover title.Includes bibliographical references (p. 41).Mod...

The Runge-Kutta equations by quadrature methods /

Rosen, Joseph S.
George C. Marshall Space Flight Center.

January 1967

"November 1967."Includes bibliographical references.Performed by George C. Marshall Space Flight Cen...

Approximate solutions of Runge-Kutta equations /

Rosen, Joseph S.
United States. National Aeronautics and Space Administration.
George C. Marshall Space Flight Center.

January 1967

Prepared at George C. Marshall Space Flight Center."August 1967"--Cover.Includes bibliographical ref...

Numerical solution of differential equations using Obrechkoff corrector formulas /

Rosen, Joseph S. (Joseph Selwyn)
United States. National Aeronautics and Space Administration.
George C. Marshall Space Flight Center.

Solution of differential equations by predictor corrector formulas for high order accuracy.Prepared ...

Numerically stable interpolation formulas with favorable error propagation for first- and second-order differential equations /

Fehlberg, Erwin.
George C. Marshall Space Flight Center.

Prepared at George C. Marshall Space Flight Center."March 1961."Cover title.Includes bibliographical...

Classical Fifth-, Sixth-, Seventh-, and Eighth-Order Runge-Kutta Formulas with Stepsize Control

Fehlberg, E.

October 1968

Runge-Kutta formulas of high order with stepsize control through leading truncation error ter

Development of a general formula expanding the higher-order derivatives of the function tanh z in powers of tanh z and A-numbers /

Hosenthien, Hans H.

Prepared at George C. Marshall Space Flight Center."January 1968"--Cover.Includes bibliographical re...

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...

Second-order small-disturbance solutions for hypersonic flow over power-law bodies /

Townsend, James C. (James Courtland), 1938-
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 57-58).Mode ...

On the error propagation of some interpolation formulas for second-order differential equations : by Erwin Fehlberg.

Fehlberg, Erwin.
George C. Marshall Space Flight Center.

Prepared at George C. Marshall Space Flight Center."July 1963"--Cover.Includes bibliographical refer...

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

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. 21-22.Mode of access: Internet

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...

Low thrust space vehicle trajectory optimization using regularized variables /

Schwenzfeger, K. J.
George C. Marshall Space Flight Center.

January 1974

Prepared at George C. Marshall Space Flight Center.Cover title.Includes bibliographical references (...

Numerical integration in a rigid-body trajectory program /

Moore, John Edd.
United States. National Aeronautics and Space Administration.
Aero-Astrodynamics Laboratory (George C. Marshall Space Flight Center)

Comparison of fourth order Runge-Kutta numerical integration technique with two numerical integratio...

The computation of partial volumes of the components in solution /

Rosen, Joseph S. (Joseph Selwyn)
George C. Marshall Space Flight Center.

Prepared at George C. Marshall Space Flight Center."December 1967"--Cover.Includes bibliographical r...

Classical eighth- and lower-order Runge-Kutta-Nyström formulas with a new stepsize control procedure for special second-order differential equations /

Abstract

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Classical eighth- and lower-order Runge-Kutta-Nyström formulas with a new stepsize control procedure for special second-order differential equations /

Abstract

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