New approaches are presented for the guidance of agile missiles. They are based an nonlinear discontinuous control techniques applied to the generation of guidance laws capable of taking advantage of the vehicle's post-stall. capabilities. Agility and maneuverability requirements imply a higher bandwidth and robustness for the guidance loop, which are addressed by a variable structure controller format. Formal stability considerations are presented, and the guidance structures are validated using nonlinear simulation.
Nonlinear guidance techniques for agile missiles
Nichtlineare Regelungsmethoden für die Flugkörperlenkung
Control Engineering Practice ; 9 , 10 ; 1131-1144
2001
14 Seiten, 21 Bilder, 1 Tabelle, 19 Quellen
Article (Journal)
English
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