Classical design and analysis techniques, many of which date back
to the 1950's, are still predominantly used in the aerospace
industry for the design and analysis of automatic flight control
and aero-engine control systems. The continued success and
popularity of these techniques is particularly impressive
considering the radical advances in aircraft and spacecraft design
and avionics technology made over this period. Clearly, an
understanding of both the advantages and limitations of these
methods is essential in order to properly evaluate the likely
usefulness of more modern techniques for the design and analysis of
aerospace control systems. One of the themes of this book is that
the multivariable robust control methods it describes are logical
and natural extensions of the more classical methods, and not
replacements for them. It is assumed that readers of this
publication are already familiar with classical flight control
techniques. Emphasis is on the philosophy, advantages and
limitations of the classical approach to flight control system
design and analysis. Abstracted in Inspec
General
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