Application of an optimal control algorithm for a gyroscope system of a homing air-to-air missile

Missile homing precision depends mainly on the correct determination of the current angle between the Gyroscope System Axis (GSA) and the target line-of-sight (LOS). A gyroscope automatic control system shall ensure spontaneous levelling of this angle, hence, constant homing of the gyroscope system...

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Bibliographic Details
Main Authors: Izabela Krzysztofik, Zbigniew Koruba
Format: Article
Published: Vilnius Gediminas Technical University 2021-04-01
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