Adaptive integrated guidance and control backstepping sliding mode design for blended control missile#br#
XIA Chuan1, DONG Chaoyang1, WANG Qing2, CHENG Haoyu3
1. School of Aeronautic Science and Engineering,Beihang University, Beijing 100191, China;
2. School of Automation Science and Electrical Engineering,Beihang University, Beijing 100191, China;
3. School of Astronautics, Northwestern Polytechnical University, Xi’an 710072, China
XIA Chuan, DONG Chaoyang, WANG Qing, CHENG Haoyu. Adaptive integrated guidance and control backstepping sliding mode design for blended control missile#br#[J]. Systems Engineering and Electronics, 2018, 40(10): 2325-2333.