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Autor(en): 
  • S. Srinathkumar
  • Eigenstructure Control Algorithms: Applications to Aircraft/Rotorcraft Handling Qualities Design 
     

    (Buch)
    Dieser Artikel gilt, aufgrund seiner Grösse, beim Versand als 3 Artikel!


    Übersicht

    Auf mobile öffnen
     
    Lieferstatus:   i.d.R. innert 14-24 Tagen versandfertig
    Veröffentlichung:  Februar 2011  
    Genre:  Naturwissensch., Medizin, Technik 
     
    Luft- und Raumfahrttechnik / TECHNOLOGY & ENGINEERING / Aeronautics & Astronautics / TECHNOLOGY & ENGINEERING / Electronics / General / TECHNOLOGY & ENGINEERING / Robotics / Technology & Industrial Arts
    ISBN:  9781849192590 
    EAN-Code: 
    9781849192590 
    Verlag:  Institution of Engineering & Technology 
    Einband:  Kartoniert  
    Sprache:  English  
    Serie:  Iee Control Engineering  
    Dimensionen:  H 240 mm / B 161 mm / D 20 mm 
    Gewicht:  621 gr 
    Seiten:  304 
    Bewertung: Titel bewerten / Meinung schreiben
    Inhalt:
    Eigenstructure control involves modification of both the eigenvalues and eigenvectors of a system using feedback. Based on this key concept, algorithms are derived for the design of control systems using controller structures such as state feedback, output feedback, observer-based dynamic feedback, implicit and explicit modelfollowing, etc. The simple-to-use algorithms are well suited to evolve practical engineering solutions.
    The design of control laws for modern fly-by-wire high performance aircraft/rotorcraft offers some unique design challenges. The control laws have to provide a satisfactory interface between the pilot and the vehicle that results in good handling qualities (HQ) in precision control tasks. This book, through detailed aircraft and rotorcraft design examples, illustrates how to develop practical, robust flight control laws to meet these HQ requirements.
    This book demonstrates that eigenstructure control theory can be easily adapted and infused into the aircraft industry's stringent design practices; therefore practicing flight control engineers will find it useful to explore the use of the new design concepts discussed. The book, being interdisciplinary in nature, encompassing control theory and flight dynamics, should be of interest to both control and aeronautical engineers. In particular, control researchers will find it interesting to explore an extension of the theory to new multivariable control problem formulations. Finally, the book should be of interest to graduate/doctoral students keen on learning a multivariable control technique that is useful in the design of practical control systems.

      



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