代表性专著、译著
[1] 《模糊控制》, 北京: 国防工业出版社, 2017.
[2] 《战术导弹制导律设计理论与方法-多约束视角》, 北京: 北京麻豆精品秘 国产传媒出版社, 2021.
[3] 《自适应控制理论与应用》(第二版), 北京: 北京麻豆精品秘 国产传媒出版社, 2022.
代表性论文：
[1] Robust partial integrated guidance and control approaches for maneuvering targets[J]. International Journal of Robust and Nonlinear Control, 2019, 29: 6522-6541.
[2] Three-dimensional terminal angle constrained robust guidance law with autopilot lag[J]. Aerospace Science and Technology, 2019, 86(3): 160-176.
[3] Neuroadaptive high-order fully-actuated system approach for roll autopilot with unknown uncertainties[J]. Aerospace Science and Technology, 2024, 155: 109567.
[4] Fractional-order ILC-based adaptive integrated guidance and control of flight vehicles with system lag[J]. Nonlinear Dynamics, 2024, 112(24): 22039-22056.
[5] Robust attitude control for hypersonic reentry vehicle via composite fixed-time stable control method[J]. Journal of the Franklin Institute, 2025, 362(1): 107426.
[6] Adaptive backstepping Impact Angle control with autopilot dynamics and acceleration saturation consideration[J]. International Journal of Robust and Nonlinear Control, 2017, 27(17): 3777-3793.
[7] Consensus-based two-stage salvo attack guidance[J]. IEEE Transactions on Aerospace and Electronic Systems, 2018, 54(3): 1555-1566.
[8] Command filtered integrated estimation guidance and control for strapdown missiles with circular field of view[J]. Defence Technology, 2024, 35: 211-221.
[9] Barrier function-based three-dimensional guidance for position-constrained interception[J]. IEEE Transactions on Aerospace and Electronic Systems, 2025, 61(2): 3782-3797.
[10] Quantized feedback neuroadaptive control for a non-affine hypersonic flight vehicles system with actuator saturation[J]. Aerospace Science and Technology, 2025, 162: 110189.
[11] Robust Second‐Order Backstepping Design of Integrated Guidance and Control Based on a Fully Actuated System Approach[J]. International Journal of Robust and Nonlinear Control, 2025, 35(8): 2933-2951.
[12] Adaptive fixed-time observer-based impact angle control guidance law for intercepting maneuvering target[J]. Aerospace Science and Technology, 2025, 158: 109871.
[13] 基于全驱系统方法的制导控制一体化设计[J]. 航空学报, 2024, 45(01): 137-149.
[14] 针对机动目标的三维领从协同制导律[J]. 兵工学报, 2024, 45(10): 3538-3554.
[15] 基于自适应扰动观测器的旋转弹神经网络过载驾驶仪设计[J]. 兵工学报, 2024, 45(11): 3841-3855.
[16] 考虑输入饱和的空间飞行器姿态神经鲁棒自适应滑模控制[J]. 宇航学报, 2024, 45(08): 1269-1280.
[17] 考虑攻击时间及空间角度约束的三维自适应滑模协同制导律设计[J]. 兵工学报, 2023, 44(09): 2778-2790.
[18]基于二阶滑模控制理论的新型滚转稳定控制器[J]. 控制与决策, 2019, 34(7): 1553-1558.
[19]考虑驾驶仪动态性能的指令滤波反演制导律[J]. 航空学报, 2020, 41(12): 332-341.
[20]大跨域条件下的自适应滚转稳定容错控制方法[J]. 航空学报, 2021, 42(03): 393-402.
