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

被引：16

作者：

Koruba, Z. ^{[1
]}

Krzysztofik, I. ^{[1
]}

Dziopa, Z. ^{[1
]}

机构：

[1] Kielce Univ Technol, Fac Mechatron & Machine Bldg, PL-25314 Kielce, Poland

来源：

BULLETIN OF THE POLISH ACADEMY OF SCIENCES-TECHNICAL SCIENCES | 2010年 / 58卷 / 04期

关键词：

missile launcher; missile rocket; gyroscope correction;

D O I：

10.2478/v10175-010-0069-4

中图分类号：

T [工业技术];

学科分类号：

08 ;

摘要：

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.

引用

页码：651 / 656

页数：6

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