A skid-to-turn missile autopilot design: The generalized predictive adaptive control approach

Author:

Bendotti P.,M'Saad M.

Publisher

Wiley

Subject

Electrical and Electronic Engineering,Signal Processing,Control and Systems Engineering

Reference27 articles.

1. ‘A comparison of six robustness tests evaluating missile autopilot robustness to uncertain aerodynamics’, Proc. ACC, San Diego, CA, 1990, pp. 755–763.

2. ‘Singular value robustness tests for missile autopilot uncertainties’, Proc. AIAA GNC Conf., 1989, pp. 1079–1089.

3. and , ‘Autopilot design for bank-to-turn missiles using the LQG/LTR methodology’, Proc. ACC, Atlanta, GA, 1988, pp. 579–586.

4. and , ‘Integrated flight/propulsion control design for a STOVL aircraft using H-infinity control design techniques’, Proc. ACC, Boston, MA, 1991, pp. 568–576.

5. and , ‘Multivariable autopilot designs for a bank-to-turn missile’, Proc. ACC, Atlanta, GA, 1988, pp. 567–572.

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