Abstract
A practical design procedure for aircraft augmentation systems based on quadratic optimal control technology and handling-quality-oriented cost functionals is described.
A practical design procedure for aircraft augmentation systems based on quadratic optimal control technology and handling-quality-oriented cost functionals is described.
In: Seventh annual conference on manual control : proceedings of a meeting held at University of Southern California, June 2-4, 1971, p. 271-284, 8 graph., 2 tab., 17 ref.
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