The research covered in this report is a result of the tasks in the control application of multivariable control theory to aircraft control laws. The report is written to provide guidelines to help control law designers use multivariable control theory for aircraft controls. The report is organized into three parts. The first included discussions on various control methodologies and presentation of fundamentals of control. The second discusses the design and analysis of controls as it relates to fighter aircraft. Finally, the third section goes through the specifics of three design methodologies using fighter aircraft for examples.
Application of Multivariable Control Theory to Aircraft Control Laws. Final Report: Multivariable Control Design Guidelines
1996
286 pages
Report
Keine Angabe
Englisch
Avionics , Navigation & Guidance System Components , Flight control systems , Control theory , Multivariate analysis , Algorithms , Computerized simulation , Software engineering , Fighter aircraft , Uncertainty , Optimization , Adaptive control systems , Pitch(Motion) , Transfer functions , Aerodynamic stability , Input output processing , Eigenvalues , Heuristic methods , Systems analysis , Flight maneuvers , Design criteria , Aircraft models , Data links , Flight simulation , Frequency response
Multivariable Control Law Design for a Tailless Aircraft
British Library Conference Proceedings | 1996
|Multivariable control design for the control reconfigurable combat aircraft (CRCA)
Tema Archiv | 1989
|Identification and reconfigurable control of multivariable aircraft
Tema Archiv | 1999
|Non-linear multivariable flight control of aircraft
SAGE Publications | 1998
|Multivariable control laws for the AFTI/F-16
AIAA | 1984
|