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Aircraft Control Allocation

W Durham (Autor)

Software / Digital Media
312 Seiten
2016
John Wiley & Sons Inc (Hersteller)
978-1-118-82778-9 (ISBN)
137,98 inkl. MwSt
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Control Allocation is a key consideration in the design of modern flight control systems and failure to properly address this results in excessive aircraft weight and system complexity, and decreased performance.

"Allocation of Redundant Controls: With Application to Airplane Flight Controls" addresses this problem and presents the mathematics and analytical techniques used to solve the control allocation as it applies to aircraft flight control. The use of highly redundant systems is discussed and the theoretical aspects of the problem and the practical applications are covered in detail. Numerous examples based on actual aircraft are included, in particular the F-15 ACTIVE flight research vehicle will be discussed. Supporting MATLAB(R) code is also available.

"Allocation of Redundant Controls: With Application to Airplane Flight Controls" is a comprehensive reference for flight control system engineers and graduate aerospace engineering students in the field of flight dynamics and control.

Wayne Durham had a full career as a U.S. Navy fighter pilot and test pilot. He is a member of the Society of Experimental Test Pilots. After retiring from the Navy he earned a Ph.D. in Aerospace Engineering at Virginia Tech, researching model-following control under the guidance of the late Fred Lutze. He remained at Virginia Tech teaching aerospace engineering and researching aircraft control, including seminal studies of control allocation. After earning his Ph.D. from Virginia Tech, Ken Bordignon spent eight years at for Lockheed Martin working on various Advanced Development Projects, including the Joint Strike Fighter Concept Demonstration Aircraft, the X-35. Since 2008 he has taught at Embry-Riddle Aeronautical University in Prescott, Arizona. Roger Beck has worked as a support contractor providing flight mechanics, simulation, guidance, navigation, and control support to NASA for a variety of aerospace projects. As part of his graduate work at Virginia Tech, Dr. Beck studied the extension of control allocation techniques to systems with more than three objectives. Working with NASA, he has supported flight tests of a variety of different vehicles including UAV flight systems, atmospheric tests of launch vehicles, hypersonic vehicles, even earth and planetary re-entry systems. In addition to flight projects, Dr. Beck provides analytical support to a variety of conceptual studies ranging ground test infrastructure to space technology demonstration missions. Currently, Dr. Beck is employed by Dynamic Concepts, Incorporated of Huntsville, Alabama, working as part of the Flight Mechanics team for the SLS launch vehicle at NASA's Marshall Space Flight Center.

Erscheint lt. Verlag 4.11.2016
Verlagsort New York
Sprache englisch
Maße 152 x 229 mm
Gewicht 666 g
Themenwelt Technik Maschinenbau
ISBN-10 1-118-82778-3 / 1118827783
ISBN-13 978-1-118-82778-9 / 9781118827789
Zustand Neuware
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