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变质心高速旋转弹的滑模姿态控制器设计

The Design of Sliding-mode Attitude Control of Variable Centroid High Spinning Projectile
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摘要 针对采用变质心技术的高速旋转弹,考虑滑块的六自由度运动,基于牛顿力学建立了由炮弹和滑块组成的多体系统的动力学模型,并根据实际情况对模型进行了合理简化。以滑块的旋转角加速度为控制量,设计了具有鲁棒性的滑模变结构姿态控制器,使弹体实际姿态角能够快速跟踪理想姿态角。 Aiming at the high spinning projectile that adopted variable centroid control,considering the moving-mass moving at six degrees of freedom,based on Newton mechanics established the more systematically model of high spinning projectile that concluding movingmass and projectile,and simplified the model based on reasonable supposition and physical truth.Taking the angular acceleration of moving-mass as control part,based on the slide mode theory,the controller that have robustness is designed.The actual attitude angel of the high spinning projectile could follow the ideal attitude angel.
作者 刘圣起 曹培培 陈峻山 谢春辉 LIU Sheng-qi;CAO Pei-pei;CHEN Jun-shan;XIE Chun-hui(Shanghai Radio Equipment Research Institute, shanghai 200090, Chin)
出处 《制导与引信》 2017年第4期5-10,共6页 Guidance & Fuze
关键词 滑模控制 变质心高速旋转弹 姿态角 sliding-mode control variable centroid high spinning projectile attitude angel
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  • 1曾颖超.战术导弹弹道与姿态动力学[M].西安:西北工业大学出版社,1991..
  • 2Raymond H B. A Moving Mass Trini Control System for Re-Entry Vehicle Guidance [ J ]. Journal of Guidance, Control, and Dynamics, 1996,19 ( 2 ) :205-216.
  • 3Sturgis. Moving Mass Trim Control for Aerospace Vehicles [J]. Journal of Guidance, Control, and Dynamics, 1996, 19(5) :1 064-1 070.

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