Rolling Control Characteristic Experimental Investigation of a Canard Missile with Free-Spinning Tail

To study the rolling control characteristics of a canard-controlled missile, a series of wind tunnel experiment is conducted. The experimental method, the structure features of wind tunnel model and the experimental results are introduced in this paper. The experimental data show that the canard is an inefficient rolling control device for canard-controlled missile with fixed tail fins; but for the free-spinning tail fin configuration, the canard can conduct rolling control of the missile, and even have higher controlling efficiency under larger canard deflection angle.

作 者： LEI Juan-mian WU Jia-sheng MENG Ling-tao   作者單位： School of Mechatronic Engineering, Beijing Institute of Technology, Beijing 100081, China  刊 名： 北京理工大學(xué)學(xué)報(bào)(英文版)  EI 英文刊名： JOURNAL OF BEIJING INSTITUTE OF TECHNOLOGY  年，卷(期)： 2006 15(1)  分類號(hào)： V211.24  關(guān)鍵詞： canard missile   aerodynamic characteristics   wind tunnel experiment   free-spinning tail   rolling control characteristics  

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