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.
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