Volume 37, Number 5, October 2019
|Page(s)||962 - 967|
|Published online||14 January 2020|
- YUN Yuhang, TANG Shengjing, GUO Jie, et al. Robust Controller Design for Compound Control Missile with Fixed Bounded Convergence Time[J]. Journal of Systems Engineering and Electronics, 2019, 29(1): 116–133 [Article] [Google Scholar]
- CHAI Dong, FANG Yangwang, WU Youli, et al. Aerodynamic Force and Lateral Thrust Blended Control for Hypersonic Missile Using Fuzzy Control Algorithm[C]//34th Chinese Control Conference, 2015: 3567–3572 [Google Scholar]
- WANG Zhengjie, LI Yangbo, LI Jing, et al. Modeling and Combined Control of Aerial Vehicle Based on Aerodynamic Force and Lateral Thrust[C]//The 2010 International Conference on Modelling, Identification and Control, 2010: 106–111 [Google Scholar]
- SHI Z, MA W, ZHANG Y, et al. Lateral Thrust and Aerodynamics Compound Control System of Missile Based on Adaptive Fuzzy Control[C]//2012 Fifth International Symposium on Computational Intelligence and Design, 2012: 231–234 [Google Scholar]
- ZHAO Mingyuan, WEI Mingying, HE Qiuru. Research on Method of Lateral Jet and Aerodynamic Fins Compound Control Based on Finite Time Stability and Backstepping Approach[J]. Journal of Astronautics, 2010, 92157–2164 [Article] (in Chinese) [Google Scholar]
- LIU Kai, SONG Xiaona, LIU Yuemin, et al. Adaptive Control for Missile Compound Control Systems[J]. Fire Control & Command Control, 2018, 43(5): 878–881 [Article] (in Chinese) [Google Scholar]
- BI Yongtao, WANG Yuhang, YAO Yu. Attitude Control Design of Missiles with Dual Control Based on Model Predictive Control and Active Disturbance Rejection Control[J]. Journal of Astronautics, 2015, 36(12): 1373–1383 [Article] (in Chinese) [Google Scholar]
- YI Jian, CHEN Yong, DONG Xinmin, et al. SQP-Based Control Allocation for Multiple Effectors with Interactions[J]. Systems Engineering and Electronics, 2016, 38(11): 2617–2623 [Article] (in Chinese) [Google Scholar]
- CHEN Xiao, WANG Xinmin, ZHOU Jian. UAV Flight Performance Optimization Based on Sequential Quadratic Programming Method[J]. Computer Simulation, 2012, 29(12): 99–102 [Article] (in Chinese) [Google Scholar]
Current usage metrics show cumulative count of Article Views (full-text article views including HTML views, PDF and ePub downloads, according to the available data) and Abstracts Views on Vision4Press platform.
Data correspond to usage on the plateform after 2015. The current usage metrics is available 48-96 hours after online publication and is updated daily on week days.
Initial download of the metrics may take a while.