Robust Multivariable Flight Control

preview-18
  • Robust Multivariable Flight Control Book Detail

  • Author : Richard J. Adams
  • Release Date : 2012-12-06
  • Publisher : Springer Science & Business Media
  • Genre : Technology & Engineering
  • Pages : 175
  • ISBN 13 : 1447121112
  • File Size : 61,61 MB

Robust Multivariable Flight Control by Richard J. Adams PDF Summary

Book Description: Manual flight control system design for fighter aircraft is one of the most demanding problems in automatic control. Fighter aircraft dynamics generally have highly coupled uncertain and nonlinear dynamics. Multivariable control design techniques offer a solution to this problem. Robust Multivariable Flight Control provides the background, theory and examples for full envelope manual flight control system design. It gives a versatile framework for the application of advanced multivariable control theory to aircraft control problems. Two design case studies are presented for the manual flight control of lateral/directional axes of the VISTA-F-16 test vehicle and an F-18 trust vectoring system. They demonstrate the interplay between theory and the physical features of the systems.

Disclaimer: www.yourbookbest.com does not own Robust Multivariable Flight Control books pdf, neither created or scanned. We just provide the link that is already available on the internet, public domain and in Google Drive. If any way it violates the law or has any issues, then kindly mail us via contact us page to request the removal of the link.

Robust Multivariable Flight Control

Robust Multivariable Flight Control

File Size : 64,64 MB
Total View : 7886 Views
DOWNLOAD

Manual flight control system design for fighter aircraft is one of the most demanding problems in automatic control. Fighter aircraft dynamics generally have hi

Robust Multivariable Flight Control

Robust Multivariable Flight Control

File Size : 21,21 MB
Total View : 3527 Views
DOWNLOAD

Manual flight control system design for fighter aircraft is one of the most demanding problems in automatic control. Fighter aircraft dynamics generally have hi