Dynamics and control of a gyroscope-stabilized platform in a ship anti-aircraft rocket missile launcher

被引：7

作者：

Koruba, Zbigniew ^{[1
]}

机构：

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

来源：

ADVANCES IN MECHATRONIC SYSTEMS, MECHANICS AND MATERIALS | 2013年 / 196卷

关键词：

dynamics and control; ship missile launcher; gyroscope-stabilized platform; SYSTEM;

D O I：

10.4028/www.scientific.net/SSP.196.124

中图分类号：

TH [机械、仪表工业];

学科分类号：

0802 ;

摘要：

The paper presents the ways of stabilising and controlling a Ship Anti-Aircraft Rocket Missile Launcher (SAARML) with the use of a Three-Axis Gyroscope-stabilized platform (TAG). The analysis of the dynamics of the SAARML and TAG systems is conducted for the case of searching and tracking a manoeuvring air target in the conditions of interferences and the influence of kinematic forces from the base (ship's deck). Some research results are presented in a graphical form.

引用

页码：124 / 139

页数：16

共 18 条

[1] DYNAMICS AND CONTROL OF A GYROSCOPE-STABILIZED PLATFORM IN A SELF-PROPELLED ANTI-AIRCRAFT SYSTEM
Koruba, Zbigniew
Dziopa, Zbigniew
Krzysztofik, Izabela
[J]. JOURNAL OF THEORETICAL AND APPLIED MECHANICS, 2010, 48 (01) : 5 - 26
[2] An analysis of the gyroscope dynamics of an anti-aircraft missile launched from a mobile platform
Koruba, Z.
Krzysztofik, I.
Dziopa, Z.
[J]. BULLETIN OF THE POLISH ACADEMY OF SCIENCES-TECHNICAL SCIENCES, 2010, 58 (04) : 651 - 656
[3] The numerical analysis of dynamics and control of a gyroscopic scanning system in an anti-aircraft missile launcher
Koruba, Zbigniew
[J]. COMMUNICATIONS IN NONLINEAR SCIENCE AND NUMERICAL SIMULATION, 2011, 16 (05) : 2230 - 2236
[4] DYNAMICS OF A CONTROLLED ANTI-AIRCRAFT MISSILE LAUNCHER MOUNTED ON A MOVEABLE BASE
Koruba, Zbigniew
Dziopa, Zbigniew
Krzysztofik, Izabela
[J]. JOURNAL OF THEORETICAL AND APPLIED MECHANICS, 2010, 48 (02) : 279 - 295
[5] Adaptive control of anti-aircraft missile launcher mounted on a mobile base
Izabela Krzysztofik
Zbigniew Koruba
[J]. Theoretical & Applied Mechanics Letters, 2012, 2 (04) : 51 - 54
[6] Adaptive control of anti-aircraft missile launcher mounted on a mobile base
Krzysztofik, Izabela
Koruba, Zbigniew
[J]. THEORETICAL AND APPLIED MECHANICS LETTERS, 2012, 2 (04)
[7] The model of dynamics and control of modified optical scanning seeker in anti-aircraft rocket missile
Gapinski, Daniel
Koruba, Zbigniew
Krzysztofik, Izabela
[J]. MECHANICAL SYSTEMS AND SIGNAL PROCESSING, 2014, 45 (02) : 433 - 447
[8] Modelling and the elements of controlled dynamics of the anti-aircraft missile launcher based onboard the warship
Dziopa, Zbigniew
Koruba, Zbigniew
[J]. MECHATRONIC SYSTEMS, MECHANICS AND MATERIALS, 2012, 180 : 269 - 280
[9] APPLICATION OF THE SLIDING CONTROLLER FOR THE GYROSCOPE SYSTEM OF THE ANTI-AIRCRAFT MISSILE
Krzysztofik, I.
Koruba, Z.
[J]. ENGINEERING MECHANICS 2017, 2017, : 530 - +
[10] Optimization of variable firing interval of anti-aircraft rocket launcher based on approximate model
Wang, Lei
Ma, Da-Wei
Zhou, Ke-Dong
[J]. Nanjing Li Gong Daxue Xuebao/Journal of Nanjing University of Science and Technology, 2012, 36 (05): : 767 - 772

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