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| Airplane Flight Dy... |
| 価格：7,720 |
| 販売元：三省堂書店 |
| Dr. Jan Roskam • ISBN10: 1-884885-18-7 • ISBN13: 9781884885181 • Softbound • 416 pgs • Reprint: 2003 In Airplane Flight Dynamics & Automatic Flight Controls, Part II, exhaustive coverage is provided of the methods for analysis and synthesis of automatic flight control systems using classical control theory. This widely used book has been updated with the latest software methods. Throughout this text, the practical (design) applications of the theory are stressed with many examples and illustrations. Aircraft stability and control characteristics are all heavily regulated by civil as well as by military airworthiness authorities for safety reasons. The role of the these safety regulations in the application of the theory is therefore stressed throughout. Airplane Flight Dynamics & Automatic Flight Controls, Part II, is an essential reference for all aeronautical engineers working in the area of stability and control, regardless of experience levels. The book minimizes reader confusion through a systematic progression of fundamentals: Elastic airplane stability and control coefficients and derivatives Method for determining the equilibrium and manufacturing shape of an elastic airplane Subsonic and supersonic numerical examples of aeroelasticity effects on stability & control derivatives Bode and root-locus plots with open and closed loop airplane applications, and coverage of inverse applications Stability augmentation systems: pitch dampers, yaw dampers and roll dampers Synthesis concepts of automatic flight control modes: control-stick steering, auto-pilot hold, speed control, navigation and automatic landing Digital control systems using classical control theory applications with Z-transforms Applications of classical control theory Human pilot transfer functions Roskam/Lan Errata SheetsABOUT THE AUTHOR:Dr. Jan Roskam has authored eleven textbooks on airplane flight dynamics and airplane design. He is the author of more than 160 papers on these topics. Dr. Roskam retired as the Ackers Distinguished Professor of Aerospace Engineering at The University of Kansas, where he taught airplane design, stability and control, in December 2003. He has actively participated in more than 36 major airplane programs. The design methodology used in Advanced Aircraft Analysis (AAA) is based on Airplane Design, Parts I - VIII, Airplane Flight Dynamics & Automatic Flight Controls, Parts I & II, and Airplane Aerodynamics and Performance. AAA incorporates and coordinates the methods, statistical databases, formulas, and relevant illustrations and drawings from these references. |
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