Open Access
| Issue |
JNWPU
Volume 37, Number 1, February 2019
|
|
|---|---|---|
| Page(s) | 41 - 47 | |
| DOI | https://doi.org/10.1051/jnwpu/20193710041 | |
| Published online | 03 April 2019 | |
- John J Spravka, Timothy R. Jorris. Current Hypersonic and Space Vehicle Flight Test and Instrumentation[C]//AIAA Flight Testing Conference, 2015, Dallas, TX [Google Scholar]
- Yan Jie, Yu Yunfeng, Fan Yonghua. Airbreathing Hypersonic Vehicle Control Technology[M]. Xi'an, Northwestern Polytechnical University Press, 2014(in chinese) [Google Scholar]
- Yan Binbin, Yan Jie. Active Disturbance Rejection Control Design for Hypersonic Vehicle[J]. Computer Measurement and Control, 2012, 20(5): 1307-1309 (in Chinese) [Article] [Google Scholar]
- Meng Zhongjie, Yan Jie. The Modeling and Fine Attitude Control for Aeroelastic Hypersonic Vehicle[J]. Journal of Astronautics, 2011, 32(8): 1683-1687 (in Chinese) [Article] [Google Scholar]
- Meng Zhongjie, Huang Panfeng, Yan Jie. Satisfying Stringent Requirements for Fine Attitude Control of Hypersonic Cruise Vehicle(HCV)[J]. Journal of Northwestern Polytechnical University, 2011, 29(3): 481-485 (in Chinese) [Article] [Google Scholar]
- Xu B. Dynamic Surface Control of Constrained Hypersonic Flight Models with Parameter Estimation and Actuator Compensation[J]. Asia Journal of Control, 2014, 16(1): 162-174 [Article] [CrossRef] [Google Scholar]
- Huo Y, Mirmirani M. Altitude and Velocity Tracking Control for an Airbreathing Hypersonic Cruise Vehicle[C]//AIAA Guidance, Navigation and Control Conference and Exhibit, Colorado, 2006 [Google Scholar]
- Fan Yonghua, Wu Xiaofei, Xu Hongyang, et al. Design of Lateral Control System for a Hypersonic Cruise missile[C]//21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, 2017 [Google Scholar]
- Fan Yonghua, Yan Pengpeng, Wang Fan, et al. Discrete Sliding Mode Control for Hypersonic Cruise Missile[J]. Discrete Dynamics in Nature and Society, 2016, 38(6): 1-10 [Article] [Google Scholar]
- Fan Yonghua, Yan Pengpeng, Xu Hongyang, et al. Lateral Control Stratrgy for a Hypersonic Cruise Missile[J]. International Journal of Advanced Robotic Systems, 2017, 14(2): 1-10 [Google Scholar]
- Xu Hongyang, Yu Yunfeng, Guo Xiaowen, et al. Four-Loop Feedback Control System with Integrator Design for Hypersonic Cruise Missile[C]//21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, 2017 [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.