Variable structure based nonlinear missile guidance and autopilot design for a direct hit with thrust vector control

Dept. of Electr. Eng., National Taiwan Univ.Yeh, Fu-KuangFu-KuangYehCheng, Kai-YuanKai-YuanChengFu, Li-ChenLi-ChenFuLI-CHEN FU2018-09-102018-09-102002http://www.scopus.com/inward/record.url?eid=2-s2.0-0036994104&partnerID=MN8TOARShttp://scholars.lib.ntu.edu.tw/handle/123456789/298275application/pdfapplication/pdfVariable structure based nonlinear missile guidance and autopilot design for a direct hit with thrust vector controlconference paper