Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
808436 | Theoretical and Applied Mechanics Letters | 2012 | 40997 Pages |
Abstract
This paper presents the problem of control of anti-aircraft missile launcher mounted on a moving carrier-vehicle. Direct excitations on the vehicle from the road cause adverse vibrations of the launcher. In order to increase the precision of the guiding system in the conditions of self-propelled movement of the setup on a bumpy road, the adaptive control algorithm was proposed. Some research results of computer simulation are presented in a graphical form.
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