supported by National Natural Science Foundation of China(Grant Nos.61622308,61873206,61933010);Open Research Project of the State Key Laboratory of Industrial Control Technology,Zhejiang University,China(Grant Nos.ICT1900312,ICT20037);Stable Supporting Fund of Science and Technology on Underwater Vehicle Technology(Grant No.SXJQR2018WDKT05);Synergy Innovation Foundation of the University and Enterprise for Graduate Students in Northwestern Polytechnical University(Grant No.XQ201904)。
This paper investigates the state-constrained controller design of a hypersonic flight vehicle(HFV)based on an asymmetric barrier Lyapunov function(ABLF).The robust adaptive back-stepping controller with integral term...
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 ...