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Design of a digital-stability augmentation and control system with gust alleviation and modal suppression

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2 Author(s)
M. Healey ; University College, Department of Electrical & Electronic Engineering, Cardiff, UK ; H. M. S. Al-Bahrani

A stochastic, discrete, implicit model-following control law is developed for a stability augmentation and control system for the pitch axis of a flexible-bodied aircraft. Particular attention is paid to the choice of weighting matrices in the quadratic i.p. so as to give a compromise between handling, gust alleviation amd modal suppression.

Published in:

Electrical Engineers, Proceedings of the Institution of  (Volume:122 ,  Issue: 4 )