×
模态框(Modal)标题
在这里添加一些文本
关闭
关闭
提交更改
取消
确定并提交
×
模态框(Modal)标题
在这里添加一些文本
关闭
×
Integrated guidance and control design for missile with terminal impact angle constraint based on sliding mode control
Peng Wu and Ming Yang
Integrated guidance and control design for missile with terminal impact angle constraint based on sliding mode control
Peng Wu and Ming Yang
Journal of Systems Engineering and Electronics . 2010, (
4
): 623 -628 . DOI: 10.3969/j.issn.1004-4132.2010.04.015