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Electric Loading Simulation System for Missile Wings and Rudders 被引量:1
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作者 齐蓉 林辉 陈明 《Defence Technology(防务技术)》 SCIE EI CAS 2006年第1期47-52,共6页
The design and the realization of missile wings and rudders loading simulation system based on digital signal processor (DSP) TMS320LF2407 and direct torque control (DTC) servo driver ACS600 are discussed. The structu... The design and the realization of missile wings and rudders loading simulation system based on digital signal processor (DSP) TMS320LF2407 and direct torque control (DTC) servo driver ACS600 are discussed. The structure and opration principle for the system are presented. Speediness and elimination of superabundant torque are two key difficulties for electric loading simulation system. The method which can eliminate the superabundant torque is researched. Test results show the airflow resistance when missile wings and rudders are spreading can be rapidly simulated with high accuracy. 展开更多
关键词 导弹 转矩 装载模拟系统 装载控制器
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