工作经历（博士后工作经历除外）：2025.09-至今 广东技术师范大学，自动化与电气工程学院，讲师 近五年主持或参加的科学研究项目/课题：哈尔滨工业大学“全驱系统理论与应用”青年研究项目，二阶全驱系统的预设性能容错控制，主持 广东省自然科学基金卓越青年团队项目，航天飞行器控制系统设计的参数引入方法，参与 深圳市基础研究面上项目，多层Markov跳跃系统分析与控制律设计，参与人 近五年主持或参加的教学研究项目/课题： 代表性成果和学术奖励情况： 1. Qin Huang(黄芩), Ying Zhang*. Predefined-time fault-tolerant control for rigid spacecraft attitude tracking maneuver with asymmetrical full-state performance constraints. Acta Astronautica, 2025, 229, 848-860. (SCI, 中科院二区) 2. Qin Huang(黄芩), Ying Zhang*. Continuous appointed‐time prescribed performance attitude tracking control for rigid spacecraft with actuator faults on SO(3)[J]. International Journal of Robust and Nonlinear Control, 2024, 34(1): 628-647.（SCI，中科院三区） 3. Qin Huang(黄芩), Ying Zhang*. Double-level prescribed performance control for rigid spacecraft attitude tracking under actuator faults[J]. Advances in Space Research, 2024, 75(4), 3950-3966. (SCI, 中科院三区) 4. Qin Huang(黄芩), Ying Zhang*. Fixed time fault tolerance attitude tracking control for spacecraft without unwinding[J]. IET Control Theory & Applications, 2023, 17(4) , 357-367.（SCI，中科院四区） 6. Qin Huang(黄芩), Ying Zhang*, Hui-Jie Sun and Jian-Bin Xiong. A Low-Complexity Fault-Tolerant Prescribed Performance Control Approach for Rigid Spacecraft Attitude Tracking[C]//2026 5th Conference on Fully Actuated System Theory and Applications (FASTA), Qinhuangdao, China, IEEE, 2026: 410-415. （EI检索） 5. Qin Huang(黄芩), Ying Zhang*. Finite-time attitude tracking for fully-actuated flexible spacecraft without angular velocity measurements[C]//2023 2nd Conference on Fully Actuated System Theory and Applications (FASTA), Qingdao, China, IEEE, 2023: 1061-1066.（EI检索） 7. 张颖，黄芩，吴爱国. 一种低复杂度的航天器抗退绕预设性能姿态跟踪控制方法，专利号： ZL202411453187.0 8. 哈尔滨工业大学“世界顶尖大学战略合作计划”联合培养博士奖学金, 2023 |
