科研获奖

1. 国防科学技术进步一等奖，2022
2. 中国仿真学会创新技术一等奖，2022.
3. 中国仪器仪表学会高等教育教学成果奖二等奖，2022.

期刊论文

1. Wei Wang, Jiaqi Liu, Shiyao Lin, Baokui Geng, Zhongjiao Shi*. Command filtered integrated estimation guidance and control for strapdown missiles with circular field of view[J]. Defence Technology, 2024, 35, 211-221.

2. Wei Wang, Yuchen Wang, Shiwei Chen, Yongcang Guo, Zhongjiao Shi*. Observer-based robust high-order fully actuated attitude autopilot design for spinning glide-guided projectiles[J]. Defence Technology, 2024, 34, 282-294.

3. Jie Zhao, Zhongjiao Shi*, Yuchen Wang, Wei Wang. Quaternion-based adaptive trajectory tracking control of a rotor-missile with unknown parameters identification[J]. Defence Technology, 2024, 31,375-386.

4. 王雨辰, 王伟, 李宁, 朱泽军, 石忠佼*. 大攻角条件下制导弹滚转稳定控制方法[J]. 兵工学报, 2024, 45(3): 774-788.

5. 石忠佼, 朱化杰, 赵良玉*, 刘志杰. 考虑舵机动力学的旋转弹自适应解耦控制[J]. 航空学报, 2022, 43(3): 325068-325068.

6. Zhekun Cheng, Liangyu Zhao, Zhongjiao Shi*. Decentralized multi-UAV path planning based on two-layer coordinative framework for formation rendezvous[J]. IEEE Access, 2022, 10: 45695 - 45708.

7. Zhongjiao Shi, Liangyu Zhao*, Zhijie Liu. Variational method based robust adaptive control for a guided spinning rockets [J]. Chinese Journal of Aeronautics, 2021, 34(3): 164-175.

8. Zhongjiao Shi, Liangyu Zhao*. Learning-based adaptive control with an accelerated iterative adaptive law[J]. Journal of The Franklin Institute, 2020, 357(10): 5831-5851.

9. Liangyu Zhao*, Zhongjiao Shi, Yeqing Zhu. Acceleration autopilot for a guided spinning rocket via adaptive output feedback[J]. Aerospace Science and Technology, 2018, 77: 573-584.

10. Zhongjiao Shi, Liangyu Zhao*, Yeqing Zhu. Robust adaptive output feedback control for a guided spinning rocket[J]. International Journal of Aerospace Engineering, 2018, 1427487.

11. Zhongjiao Shi, Liangyu Zhao*. Robust model reference adaptive control based on linear matrix inequality[J]. Aerospace Science and Technology, 2017, (66): 152-159.

12. Zhongjiao Shi, Liangyu Zhao*. Effects of aeroelasticity on coning motion of a spinning missile[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2016, 230(14): 2581-2595.

13. 石忠佼, 谢浩怡, 林蔚, 赵良玉*. 单通道控制的旋转弹锥形运动稳定性研究[J].固体火箭技术, 2015, (02):156-159.

会议论文

1. Hao Xu, Liangyu Zhao, Zhongjiao Shi*. Robust Adaptive Control for Safety-Critical Systems via Control Barrier Functions[C]. 2022 China Automation Congress (CAC), 1745-1749, Xiamen, China, 2022.

2. Huajie Zhu, Zhongjiao Shi*, Liangyu Zhao. Trajectory Tracking of a Quadrotor Missile via Adaptive Backstepping Control[C]. 2022 37th Youth Academic Annual Conference of Chinese Association of Automation, Beijing China, 2022.

3. Huajie Zhu, Zhongjiao Shi*, Liangyu Zhao. Memory-augmented adaptive control with parameter convergence guarantee[C]. 2021 Chinese Automation Congress, Beijing, China, 2021.

4. Zhongjiao Shi, Liangyu Zhao*, Yong Zhao, Fengjie Gao. Transient performance analysis of adaptive control with control architecture modification[C]. 2019 Chinese Automation Congress, Hangzhou, China, 2019.

5. Zhongjiao Shi, Liangyu Zhao*. Adaptive output feedback autopilot design for spinning projectiles[C].The 36th Chinese Control Conference, Dalian, China, 2017.

6. Zhongjiao Shi, Liangyu Zhao*. On the autopilot design for a quadrotor during landing phase[C]. The 35th Chinese Control Conference, Chengdu, China, 2016.

7. Zhongjiao Shi, Liangyu Zhao*. Coning motion instability of a spinning missile induced by aeroelasticity[C]. AIAA Atmospheric Flight Mechanics Conference, San Diego, CA, USA, 2016.

*代表通讯作者

专著、译著

1. 石忠佼, 程喆坤, 朱化杰等. 无人飞行系统设计[M]. 北京: 机械工业出版社, 2022. (翻译自 Mohammad H. Sadraey Design of Unmanned Aerial Systems [M]. Wiley & Sons Ltd, 2019)

2. 赵良玉, 石忠佼. 模型参考自适应控制导论[M]. 北京: 机械工业出版社, 2019. (翻译自 Nhan T. Nguyen. Model-Reference Adaptive Control–A Primer [M]. Springer International Publishing AG 2018.)