Gao, Shaowu
Yang, Changyong
Xu, Jiuhua
Su, Hao
Fu, Yucan
Ding, Wenfeng
Funding for this research was provided by:
National Natural Science Foundation of China (51305200)
Special Research Project of Civil Aircraft (MJ-2015-G-087)
Jiangsu Key Laboratory of Advanced Numerical Control Technology (KXJ201502)