Application of optimal control and filtering theory to controller design for a bank-to-turn missile operating under CLOS guidance is described. One approach is based on two identical single-plane compensators. The second problem fromulation involves direct choice of lift force magnitude and orientation. The effect of constraining the roll rate is discussed for both fixed-and variable-wing-angle configurations.
Design of controllers for bank-to-turn CLOS guidance using optimal control
Entwurf von Reglern fuer optimale Steuerung von Kurzstreckenraketen
Proc. of the 1986 American Control Conf. ; 2 ; 1143-1148
1986
6 Seiten, 7 Bilder, 2 Tabellen, 7 Quellen
Conference paper
English
Digital controllers for bank-to-turn CLOS guidance
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