Open Access
| Issue |
JNWPU
Volume 37, Number 3, June 2019
|
|
|---|---|---|
| Page(s) | 523 - 531 | |
| DOI | https://doi.org/10.1051/jnwpu/20193730523 | |
| Published online | 20 September 2019 | |
- ZhuJihong, ZhangShangmin, ZhouChijun, et al. Dynamic Characteristics and Challenges for Control System of Super-Maneuverable Aircraft[J]. Control Theory & Applications, 2014, (12): 1650-1662 [Article] [Google Scholar]
- WangQing, QianWeiqi, DingDi. A Review of Unsteady Aerodynamic Modeling of Aircrafts at High Angles of Attack[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(8): 2331-2347 [Article] [Google Scholar]
- SnellS A, DaleF N, WilliamL A. Nonlinear Inversion Flight Control for a Supermaneuverable Aircraft[J]. Journal of Guidance Control and Dynamics, 1990, 15(4): 976-984 [Article] [Google Scholar]
- Wu F, Gopalarathnam A, Kim S. Post-Stall Aerodynamic Modeling and Gain-Scheduled Control Design[C]//AIAA Guidance, Navigation, and Control Conference and Exhibit, 2005: 6169 [Google Scholar]
- ZhuJiaqiang, GuoSuofeng. Neural-Net Based Adaptive Reconfigurable Control for a Super-Maneuverable Aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2003, 24(3): 246-250 [Article] [Google Scholar]
- LiuShuguang, SunXiuxia, DongWenhan. Design of Post-Stall Maneuvering Flight Control Law Based on Dynamic Surface Control[J]. Systems Engineering & Electronics, 2010, 28(6): 41-44 [Article] [Google Scholar]
- WuD, ChenM, GongH. Robust Control of Post-Stall Pitching Maneuver Based on Finite-Time Observer[J]. ISA Transactions, 2017, 70: 53-63 [Article] [CrossRef] [Google Scholar]
- FanZiqiang, FangZhenping Robust, Nonlinear Control Design for a Poststall Maneuver Aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2002, 23(3): 193-196 [Article] [Google Scholar]
- TolH J, De VisserC C, Van KampenE, et al. Nonlinear Multivariate Spline-Based Control Allocation for High-Performance Aircraft[J]. Journal of Guidance, Control, and Dynamics, 2014, 37(6): 1840-1862 [Article] [NASA ADS] [CrossRef] [Google Scholar]
- Atesoglu, Zgren M K. Nonlinear Robust Controller Design for High-Alpha Maneuvering Enhancement of a Fighter Aircraft with Aerodynamic and Thrust Vectoring Controls[C]//AIAA Guidance, Navigation and Control Conference and Exhibit, 2008: 6488 [Google Scholar]
- Dwivedi P N, Bhale P G, Bhattacharya A, et al. State Estimation Using UKF and Predictive Guidance for Engaging Barrel Roll Aircrafts[C]//American Control Conference, 2013: 6175-6180 [Google Scholar]
- LiuChunming, ZhaoZhijun, BuChen, et al. Double Degree-of-Freedom Large Amplitude Motion Test Technology in Low Speed Wind Tunnel[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(8): 2417-2425 [Article] [Google Scholar]
- LyuY, ZhangW, ShiJ, et al. Unsteady Aerodynamic Modeling of Biaxial Coupled Oscillation Based on Improved ELM[J]. Aerospace Science & Technology, 2017, 60: 58-67 [Article] [NASA ADS] [CrossRef] [Google Scholar]
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