摘要:In this paper a classical feedback controller has been designed to furnish fast
acting characteristics in the face of parametric perturbation using two
parameters, Generalized Time Constant and Characteristic Ratios. The design is
extended to develop a controller for the pitch control of a BRAVO fighter
aircraft. This design allows reduction of overshoot, control of speed of the
response and robust stability with parametric perturbation.
关键词:characteristic ratios, generalized time constant, Butterworth polynomial,
overshoot reduction.