Add to ORKGCaption title.Bibliography: leaf [12].Supported, in part, by a grant from the NASA Ames and Langley Research Centers. NASA/NAG-2-297 Supported, in part, by a contract from the Office of Naval Research. ONR/N00014-82-K-0582 (NR 606-003) Supported, in part, by a grant from the AFOSR-Eglin A.FB. F08635-87-K-0031 Supported, in part, by a grant from the National Science Foundation. NSF/ECS-8210960David A. Milich, Michael Athans, Lena Valavani, and Gunter Stein
This edition is a revised and expanded version of the first edition, which was published in 1996. It...
This edition is a revised and expanded version of the first edition, which was published in 1996. It...
The main motivation for the work under the present grant was to use nonlinear feedback linearization...
Caption title.Includes bibliographical references.Supported by the NASA Ames and Langley Research Ce...
A new methodology is developed for the synthesis of linear, time-invariant (LTI) controllers for mul...
Bibliography: leaf 8.Caption title. Supported in part by the Fannie and John Hertz Foundation.NASA A...
Caption title.Includes bibliographical references (leaves 38-41).Research supported by the NSF. 9157...
Caption title.Bibliography: p. 37-38.Supported in part by the General Electric Corporate Research an...
Stability margin for multiloop flight control systems has become a critical issue, especially in hig...
Bibliography: leaf 6.Supported by the NASA Ames and Langley Research Centers under grant NASA/NAG 2-...
A method is developed to design a fixed-parameter compensator for a linear, time-invariant, SISO (si...
Includes bibliographical references (leaf 12).Research supported by the National Science Foundation....
The robustness of control systems with respect to model uncertainty is considered using simple frequ...
This edition is a revised and expanded version of the first edition, which was published in 1996. It...
This edition is a revised and expanded version of the first edition, which was published in 1996. It...
This edition is a revised and expanded version of the first edition, which was published in 1996. It...
This edition is a revised and expanded version of the first edition, which was published in 1996. It...
The main motivation for the work under the present grant was to use nonlinear feedback linearization...
Caption title.Includes bibliographical references.Supported by the NASA Ames and Langley Research Ce...
A new methodology is developed for the synthesis of linear, time-invariant (LTI) controllers for mul...
Bibliography: leaf 8.Caption title. Supported in part by the Fannie and John Hertz Foundation.NASA A...
Caption title.Includes bibliographical references (leaves 38-41).Research supported by the NSF. 9157...
Caption title.Bibliography: p. 37-38.Supported in part by the General Electric Corporate Research an...
Stability margin for multiloop flight control systems has become a critical issue, especially in hig...
Bibliography: leaf 6.Supported by the NASA Ames and Langley Research Centers under grant NASA/NAG 2-...
A method is developed to design a fixed-parameter compensator for a linear, time-invariant, SISO (si...
Includes bibliographical references (leaf 12).Research supported by the National Science Foundation....
The robustness of control systems with respect to model uncertainty is considered using simple frequ...
This edition is a revised and expanded version of the first edition, which was published in 1996. It...
This edition is a revised and expanded version of the first edition, which was published in 1996. It...
This edition is a revised and expanded version of the first edition, which was published in 1996. It...
This edition is a revised and expanded version of the first edition, which was published in 1996. It...
The main motivation for the work under the present grant was to use nonlinear feedback linearization...