The guidance and control problem for tactical air-to-air missiles is addressed using a modern control theory approach. The autopilot is designed based upon a generalized formulation of the optimal tracker to provide both airframe stability and command following from the guidance signals, and the guidance law is designed using the optimal regulator. Associated implementation issues are discussed.
An integrated approach to the guidance and control of tactical missiles
Eine integrierte Loesung zur Fuehrung und Steuerung von taktischen Flugkoerpern
Proc. of the 22nd IEEE Conf. on Decision and Control ; 3 ; 1304-1309
1983
6 Seiten, 2 Bilder, 3 Tabellen, 7 Quellen
Conference paper
English
Guidance and control of tactical missiles
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