发表论文
1. Jiangtao Xu, Ya Yang, Bangsheng Fu, Shaobo Wang, Quanxi Gao. Dynamics analysis of slender vehicle influenced by random factors[J]. Journal of Fluids and Structures, 2020, 97: 10386.
2. Jiangtao Xu, Ya Yang, Bangsheng Fu, Dewei Zhang. Modeling and analysis of long booster clustered launch-vehicle[J]. Scientific Reports, 2020, 10(1): 1-12.
3. Dewei Zhang, Hui Qi, Jiangtao Xu, Ya Yang. Modeling and Analysis of Aeroelasticity and Sloshing for Liquid Rocket [J]. IEEE Access. 2019, 7: 4453-4465.
4. Bangsheng Fu, Hui Qi, Jiangtao Xu, Ya Yang. Attitude Control in Ascent Phase of Missile Considering Actuator Non-Linearity and Wind Disturbance[J]. Applied Sciences. 2019, 9(23): 5113-5122.
5. Jiangtao Xu, Na Luo, Ya Yang, Pengxin Han, Dewei Zhang. Reliability Analysis for the Hydraulic Booster Control Surface of Aircraft[J]. Journal of Aircraft, 2017, 54(2):1-8.
6. Jiangtao Xu, Yu Fu, Ganghui Cao, Ya Yang. Adaptive NN backstepping with considering integral of tracking error [J]. IEEE Access. 2020, 8(99).
7. Jiangtao Xu, Na Luo, Bangsheng Fu, et al. Checking unscented information fusion algorithm for autonomous navigation vehicles[J]. Optik, 2019, 179: 1140-1151.
8. Jiangtao Xu, Na Luo, Shaojie Liu, et al. Research on component synthesis active vibration suppression method for flexible spacecraft attitude maneuver with reaction jet actuators[J]. Aircraft Engineering and Aerospace Technology, 2020, 92(2):256-263.
9. Bin Liu，Jiangtao Xu，Bangsheng Fu，Yong Hao，Tianyu An. A covariance shaping filtering method for tightly-coupled MIMU/GNSS of UAV[J]. Aircraft engineering and aerospace technology, 2019.
10. Xu J, Luo N, Fu Y, et al. Research on RBV Control Strategy of Large Angle Maneuver[J]. Abstract and Applied Analysis,2014,(2014-1-28), 2014, 2014(1):1-11.
12. Xu J, Qi H, Chen W, et al. Reusable boosted vehicle attitude controller design[J]. Aircraft Engineering & Aerospace Technology, 2013, 85(5):415-421.
13. Xu J, Luo N, Yang Y, et al. Raliability Analysis for the Hydraulic Booster control Surface of Aircraft[J]. Journal of Aircraft.2016.11.
14. Xu J, Qi H, Chen W, et al. Modeling and Controller Designing on the Large Attitude Adjusting Phase of Reusable Boosted Vehicle[C]// International Conference on Industrial Control and Electronics Engineering. IEEE, 2012:1295-1299.
15. Xu J, Cui N, Chen Y, et al. Research on control allocation based on improved fixed-point for reusable boosted vehicle[J]. Acta Aeronautica Et Astronautica Sinica, 2012, 33(12):2268-2278.
16. Xu J, Cui N, Tian J, et al. Study on dynamic decoupling design by using INA method for cruise missile[C]// International Symposium on Systems and Control in Aerospace and Astronautics. IEEE, 2008:1-5.
17. Cui N G, Xu J, Mu R, et al. Gain-scheduled reusable launch vehicle attitude controller design[C]// International Conference on Mechatronics and Automation. IEEE, 2009:4393-4397.
18. Xia G, Dong R, Xu J, et al. Linearized Model of Carrier-Based Aircraft Dynamics in Final-Approach Air Condition[J]. Journal of Aircraft, 2015, 53(1):1-15.
19. Zhou W, Wang H, Xu J, et al. Design of the Reusable Boosted Vehicle’s (RBV) Control Allocation in the Reentry Process[M]// Theory, Methodology, Tools and Applications for Modeling and Simulation of Complex Systems. Springer Singapore, 2016.
20. Yang F, Wei C, Cui N, et al. Adaptive generalized super-twisting algorithm based guidance law design[C]// International Workshop on Variable Structure Systems. IEEE, 2016:47-52.
21. Wei C, Guo J, Park S Y, Xu J, et al. IFF Optimal Control for Missile Formation Reconfiguration in Cooperative Engagement[J]. Journal of Aerospace Engineering, 2013, 28(3):04014087.
22. 许江涛, 崔乃刚, 路菲,等. 无人机非方阵系统解耦控制[J]. 航空学报, 2008(b05):157-162.
23. 许江涛, 崔乃刚, 穆荣军. 基于Elman网络结构的惯导平台漂移模型辨识方法[J]. 系统工程与电子技术, 2010, 32(7):1497-1500.
24. 许江涛, 崔乃刚, 吕世良. 协调增益调度的重复使用助推器姿态控制设计[J]. 光学精密工程, 2010, 18(12):2590-2596.
25. 许江涛, 崔乃刚, 陈阳阳,等. 基于改进定点二乘的重复使用助推飞行器控制分配研究[J]. 航空学报, 2012, 33(12):2268-2278.
26. 许江涛, 陈阳阳, 吴限德,等. 重复使用助推飞行器大调姿段控制器设计[J]. 控制工程, 2013, 20(3):493-496.
27. 齐辉, 张泽, 许江涛,等. 基于Nussbaum增益滑模自适应控制的导弹制导控制一体化设计[J]. 控制与决策, 2017, 32(1):93-99.
28. 齐辉, 张泽, 许江涛,等. 基于反演滑模控制的导弹制导控制一体化设计[J]. 系统工程与电子技术, 2016, 38(3):618-623.
29. 周晚萌, 王华, 许江涛,等. 基于线性相关系数的RBV再入段增益调度设计[J]. 弹道学报, 2014(4):1-6.
30. 夏桂华, 董然, 许江涛,等. 考虑扰流的舰载机终端进场线性模型[J]. 航空学报, 2016, 37(3):970-983.
31. 白瑜亮, 崔乃刚, 郭继峰,许江涛,等. 基于隐式增量动态逆的水下运载器出水姿态控制[J]. 兵工学报, 2013, 34(7):922-928.
32. 陈卫东, 陈阳阳, 薛志霞,许江涛,等. 基于双滑模变结构的巡航导弹纵向控制系统设计[J]. 航空计算技术, 2013, 43(1):4-8.
33. 崔乃刚, 白瑜亮, 常亚武,许江涛,等. 基于非线性动态逆的水下运载器控制方法研究[J]. 兵工学报, 2013, 34(4):443-450.
34. 杨赧, 穆荣军, 崔乃刚,许江涛,等. 可重复使用助推器调姿转弯段的控制系统设计[J]. 上海航天, 2012, 29(5):36-40.
