supported by National Natural Science Foundation of China(Grant Nos.61473124,61203081,61174079);Doctoral Fund of Ministry of Education of China(Grant No.20120142120091);Precision Manufacturing Technology and Equipment for Metal Parts(Grant No.2012DFG70640)
The dynamic decoupling problem of the hypersonic flight vehicle (HFV) is considered in this paper. The Linear Parameter-Varying (LPV) model of the HFV is firstly obtained and smoothly transformed into a polytopic ...