摘要
FL24风洞在国内首次进行了带控制律的CTS试验,这是改进捕获轨迹试验方式的一次探索。文中对国内外研究现状、试验技术原理、实现过程进行了阐述。试验结果表明在加控制律的CTS试验中导弹的滚转角和偏航角输出趋稳,呈有控状态。
The CTS test with control law has been firstly applied in FL24 wind tunnel in our country, which was the search on improving CTS test way. In this paper, the current situation, the principle and the realization process are introduced. The preliminary result has suggested that the rolling angle and yawing angle are steady in the test with control law.
出处
《流体力学实验与测量》
CSCD
北大核心
2003年第1期24-27,共4页
Experiments and Measurements in Fluid Mechanics
