BULLETIN of the

POLISH ACADEMY of SCIENCES

TECHNICAL SCIENCES

BULLETIN of the POLISH ACADEMY of SCIENCES: TECHNICAL SCIENCES
Volume 58, Issue 4, December 2010

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pp 651 - 656

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An analysis of the gyroscope dynamics of an anti-aircraft missile launched from a mobile platform

Z. KORUBA, I. KRZYSZTOFIK, and Z. DZIOPA
The work considers the effect of the kinematic action resulting from the basic motion of the vehicle on the dynamics of the launcher and the gyroscope acting as the drive of the opto-electro-mechanical target coordinator in a self-guided missile. The problem was analyzed using a hypothetical short-range anti-aircraft system. The simulation results were represented graphically.
Key words:

missile launcher, missile rocket, gyroscope correction


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