Design of a Helicopter Autopilot by Means of Linearizing Transformations

Design of a Helicopter Autopilot by Means of Linearizing Transformations
Title Design of a Helicopter Autopilot by Means of Linearizing Transformations PDF eBook
Author
Publisher
Pages 18
Release 1982
Genre
ISBN

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Application and Flight Test of Linearizing Transformations Using Measurement Feedback to the Nonlinear Control Problem

Application and Flight Test of Linearizing Transformations Using Measurement Feedback to the Nonlinear Control Problem
Title Application and Flight Test of Linearizing Transformations Using Measurement Feedback to the Nonlinear Control Problem PDF eBook
Author Robert F. Antoniewicz
Publisher
Pages 60
Release 1991
Genre Airplanes
ISBN

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports
Title Scientific and Technical Aerospace Reports PDF eBook
Author
Publisher
Pages 256
Release 1990
Genre Aeronautics
ISBN

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NASA Technical Paper

NASA Technical Paper
Title NASA Technical Paper PDF eBook
Author
Publisher
Pages 60
Release 1991
Genre Science
ISBN

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NASA Technical Paper

NASA Technical Paper
Title NASA Technical Paper PDF eBook
Author United States. National Aeronautics and Space Administration
Publisher
Pages 168
Release 1991
Genre Aeronautics
ISBN

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Nonlinear Control Systems and Power System Dynamics

Nonlinear Control Systems and Power System Dynamics
Title Nonlinear Control Systems and Power System Dynamics PDF eBook
Author Qiang Lu
Publisher Springer Science & Business Media
Pages 398
Release 2013-04-17
Genre Mathematics
ISBN 1475733127

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Nonlinear Control Systems and Power System Dynamics presents a comprehensive description of nonlinear control of electric power systems using nonlinear control theory, which is developed by the differential geometric approach and nonlinear robust control method. This book explains in detail the concepts, theorems and algorithms in nonlinear control theory, illustrated by step-by-step examples. In addition, all the mathematical formulation involved in deriving the nonlinear control laws of power systems are sufficiently presented. Considerations and cautions involved in applying nonlinear control theory to practical engineering control designs are discussed and special attention is given to the implementation of nonlinear control laws using microprocessors. Nonlinear Control Systems and Power System Dynamics serves as a text for advanced level courses and is an excellent reference for engineers and researchers who are interested in the application of modern nonlinear control theory to practical engineering control designs.

Control and Dynamic Systems V38: Advances in Aeronautical Systems

Control and Dynamic Systems V38: Advances in Aeronautical Systems
Title Control and Dynamic Systems V38: Advances in Aeronautical Systems PDF eBook
Author C.T. Leonides
Publisher Academic Press
Pages 420
Release 2012-12-02
Genre Transportation
ISBN 032316286X

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Advances in Aeronautical Systems shows that real-time simulation of aeronautical systems is fundamental in the analysis, design, and testing of today's increasingly complex aeronautical systems. Perhaps more important is the fact that simulation, including 3-D vision and motion simulation techniques, is an essential element in pilot training for both commercial and military aircraft. An essential characteristic of all modern aeronautical systems is their avionics system, which is composed of many elements, in particular sensor systems. This book comprises eight chapters, with the first focusing on aircraft automatic flight control system with model inversion. The following chapters then discuss information systems for supporting design of complex human-machine systems and formulation of a minimum variance deconvolution technique for compensation of pneumatic distortion in pressure-sensing devices. Other chapters cover synthesis and validation of feedback guidance laws for air-to-air interceptions; multistep matrix integrators for real-time simulation; the role of image interpretation in tracking and guidance; continuous time parameter estimation: analysis via a limiting ordinary differential equation; and in-flight alignment of inertial navigation systems. This book will be of interest to practitioners in the fields of engineering and aeronautics.