摘要
以某型号反坦克导弹舵机为对象,对一种称之为微力矩负载模拟器进行了研究。根据该型号导弹舵机的特点,对系统关键元件的选择设计进行了分析,建立了系统的数学模型,并通过分析多余力矩的产生机理,对系统进行了多余力矩补偿和校正,最后进行了仿真分析。
The micro-moment load simulator of an antitank missile is investigated. According to the characteristic of the missile rudder, the selecting and design of the system＇s key parts are analyzed, and the system mathematic model is built. By analyzing the mechanism of production of the extraneous torque, the extraneous torque compensation and adjustment are made. At last, the simulations and its analyzing are conducted.
出处
《中国惯性技术学报》
EI
CSCD
2005年第6期54-57,共4页
Journal of Chinese Inertial Technology
