An H <sup>∞</sup>-based control system design
procedure is developed to produce a controller in which the closed-loop
system is designed, using H <sup>∞</sup> controller in
which the closed-loop system is designed, using H <sup>∞
</sup> methods similar to those of H. Kwakernaak (1986), to be robust
with respect to both disturbance rejection and insensitivity to
parameter variations. The H
... [Show full abstract] <sup>∞</sup> design approach
is coupled with multicriterion optimization to design a pitch-axis
controller for the F-14 aircraft, (a version of a benchmark problem).
The authors design a discrete-time controller even though the benchmark
is in continuous time. The benchmark, while specifying gain and phase
margins, does not specify the expected ranges for the parameters of the
plant. Estimates have been obtained of the reasonable ranges of
parameter variations, which are checked against the design. The
precompensator is used to shape the output response so as to cause the
entire system to achieve the desired performance. The robustness of the
angle-of-attack response under large parameter variations is examined. A
satisfactory design has not yet been obtained. However, these
intermediate results are thought to be of value in demonstrating the
difficulty of the problem and the thought processes involved in trying
to use H <sup>∞</sup> methods to solve a realistic design
problem