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矢量控制反坦克导弹重力补偿设计
引用本文:侯师,张靖,朱湘龙. 矢量控制反坦克导弹重力补偿设计[J]. 江南大学学报(自然科学版), 2012, 11(4): 487-491
作者姓名:侯师  张靖  朱湘龙
作者单位:北京理工大学机电学院,北京,100081
摘    要:针对矢量控制的反坦克导弹,提出了一种基于导弹飞行物理过程、从导弹系统整体角度出发求取重力补偿的方法。通过仿真验证了该方法的可行性,并与传递函数法作了比较。这种方法一定程度上避免了孤立以某一主要影响因子分段求取重补指令,因此更加简便,同时可靠。

关 键 词:矢量控制  反坦克导弹  物理过程  重力补偿

Design of Gravity Compensation for Anti-Tank Missile with Vector Control
HOU Shi , ZHANG Jing , ZHU Xiang-long. Design of Gravity Compensation for Anti-Tank Missile with Vector Control[J]. Journal of Southern Yangtze University:Natural Science Edition, 2012, 11(4): 487-491
Authors:HOU Shi    ZHANG Jing    ZHU Xiang-long
Affiliation:(School of Mechatronical Engineering,Beijing Institute of Technology,Beijing 100081,China)
Abstract:Addressing an anti-tank missile with vector control,this paper puts forward a new way to solve gravity compensation based on the physical process of the missile in flight and also considering from a whole view on the missile system.We have validated the feasibility by emulator and then drawn a conclusion that this method is more convenient and reliable than the way of transfer function methods.To a certain extent,the method avoids taking only certain primary impact factors into account and solving gravity compensation in a segmented way.
Keywords:vector control  anti-tank missile  physics process  gravity compensation
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