图书章节：
(1)《先进复合材料飞机结构设计与应用》（第八章：复合材料结构优化设计），航空工业出版社，2019
(2)唐胜景、郭杰、李响，《Introduction to flight vehicle system（飞行器系统概论）》，国防工业出版社，2012
期刊论文：
(1)刘旭，李响等，高超声速滑翔飞行器解析协同再入制导，宇航学报，2023，44（5）：731-742
(2)李响，贾欲明，洪润民，Hashin准则的应力应变形式在复合材料渐进损伤计算中的对比，机械工程学报，2022，58（22）：284-293
(3)朱璐，李响等，星箭分离减冲击环结构优化设计，宇航学报，2022，43（7）：946-956
(4)刘旭, 李响, 张后军等，不确定条件下采用协方差描述函数法的再入轨迹鲁棒优化，宇航学报，2021，42（11）：1404-1415
(5)洪润民，李响，丁继锋，采用伪速度冲击响应谱评估蜂窝夹层板破坏边界，宇航学报，2020， 41 (9): 1151-1157
(6)Yuheng Guo, Xiang Li, Houjun Zhang, Entry Guidance With Terminal Time Control Based on Quasi-Equilibrium Glide Condition, IEEE Transactions on Aerospace and Electronic Systems, 2020, 56(2): 887-896.
(7)Yuheng Guo, Xiang Li, Houjun Zhang, Data-Driven Method for Impact Time Control Based on Proportional Navigation Guidance, AIAA Journal of Guidance, Control, and Dynamics, 2020, 43(5): 955-966.
(8)Xiang Li, Hui He, Hongqiang Ma, Structure design of six-component strain-gauge-based transducer for minimum cross-interference via hybrid optimization methods, Structural and Multidisciplinary Optimization，2019, 60(1):301-304
(9)宋文斌，李响，王晓鹏，左英桃, 基于参数化气动模型的机载导弹分离轨迹优化,空气动力学学报，2018，36(1): 35-40
(10)Xiang Li; Xiaopeng Wang; Houjun Zhang; Trajectory Optimization Using Analytical Target Cascading, ASME Journal of Mechanical Design, 2017, 139(12).
(11)Xiang Li; Prasanth B. Nair; ZhiGang Zhang; Aircraft Robust Trajectory Optimization Using Nonintrusive Polynomial Chaos, AIAA Journal of Aircraft, 2014, 51 (5): 1592-1603.
(12)Xiang Li; ChangAn Liu; Weiji Li; Application of Collaborative Optimization to Optimal Control Problems, AIAA Journal, 2013, 51(3): 744-750
