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SCI源：
Ju Xiaozhe, Wei Changzhu, Zhang Liang, et al. Semi-globally smooth control for VTVL reusable launch vehicle under actuator faults and attitude constraints[J]. Acta Astronautica, 2021.
Wei Changzhu,Wang Ruiming,Zheng Wei,Pu Jialun. Equivalent dynamic modeling of flexible morphing aircraft.[J]. Science progress,2021,104(2):
Zhang Chenxin,Zhang Yankun,Wei Changzhu,Pecora Rosario. Onboard Trajectory Generation of Hypersonic Morphing Aircraft[J]. International Journal of Aerospace Engineering,2021,2021:
Li Yuan,Wei Changzhu,He Yanfeng,Hu Renyi. A convex approach to trajectory optimization for boost back of vertical take-off/vertical landing reusable launch vehicles[J]. Journal of the Franklin Institute,2021,358(7):
Jing Liang,Wei Changzhu,Zhang Liang,Cui Naigang,Ben Makhlouf Abdellatif. Cooperative Guidance Law with Predefined-Time Convergence for Multimissile Systems[J]. Mathematical Problems in Engineering,2021,2021:
Chenxin Zhang, Yankun Zhang, Changzhu Wei, et al. Onboard Rocket Landing Guidance Using Convex Optimization and Model Predictive Control.[J]. International Journal of Aerospace Engineering,Volume 2021. (SCI 检索)
Wei Chang Zhu,Zhang Ze,Li Yuan,Li Yongyuan. Multi-Process Integrated Planning and Guidance for Return of Reusable Aircraft Under Time Constraint[J]. IEEE ACCESS,2020,8:
Yuan Li ,Baojun Pang , Changzhu Wei, et al. Online trajectory optimization for power system fault of launch vehicles via convex programming [J]. Aerospace Science and Technology, 98: 105682, 2020. (SCI 检索)
Yuan Li ,Wei Changzhu,Baogang Lu , et al.Improved guidance algorithm considering terminal attitude constraints for spacecrafts via optimal control theory [J]. Optimal Control Applications & Methods, 2020. (SCI 检索)
Huibing Shao ,Yepeng Han ,Changzhu Wei , et al.A Novel Recurrent Convolutional Neural Network-Based Estimation Method for Switching Guidance Law [J]. Ieee Access, 10159-10168,2020. (SCI 检索)
Chenhao Zhu ,Wei Chang zhu, Guodong Xu , et al.Impact-Time-Control Guidance Law for Hypersonic Missiles in Terminal Phase [J]. Ieee Access, 8, 44611-44621,2020. (SCI 检索)
Changzhu Wei ,Ju Xiaozhe, Rong Wu , et al. Geometry and time updaters-based arbitrary-yaw iterative explicit guidance for fixed-thrust boost back of vertical take-off/vertical landing reusable launch vehicles [J].Aerospace Science and Technology, 95: 105433, 2019. (SCI 检索)
Liang Zhang , Changzhu Wei ,Rong Wu ,et al. Adaptive fault-tolerant control for a VTVL reusable launch vehicle [J]. Engineering Aerospace, AEROSPACE, 159: 362-370, 2019. (SCI 检索)
Liang Zhang, Changzhu Wei, Rong Wu , et al. Fixed-time adaptive model reference sliding mode control for an air-to-ground missile [J]. Chinese Journal Of Aeronautic, 32(5): 1268-1280, 2019. (SCI 检索)
Jinbo Wang ,Naigang Cui , Changzhu Wei, et al. Optimal Rocket Landing Guidance Using Convex Optimization and Model Predictive Control [J]. Chinese Journal Of Aeronautic, 42(5): 1078-1092, 2019. (SCI 检索)
Jinbo Wang , Naigang Cui , Changzhu Wei ,et al. Optimal Rocket Landing Guidance Using Convex Optimization and Model Predictive Control[J]. Journal of Mathematics,2019.(SCI检索)
JinboWang ,Naigang Cui , Changzhu Wei, et al. Rapid trajectory optimization for hypersonic entry using a pseudospectral-convex algorithm [J]. Proceeding Of The Institution Of Mechanicak Engineers Part G-Journal Of Aerospace Engineering, 233(14): 5227-5238, 2019. (SCI 检索)
Yuan Li, Yingzi Guan , Wei Changzhu, et al. Optimal Control of Ascent Trajectory for Launch Vehicles: A Convex Approach [J]. Ieee Access, 7: 186491-186498, 2019. (SCI 检索)
Liang Zhang, Changzhu Wei, Yin Diao ,et al. On-line orbit planning and guidance for advanced upper stage [J]. Aircraft Engineering And Aerospace Technology, 91(4): 634-647, 2019. (SCI 检索)
Jinbo Wang ,Naigang Cui ,Changzhu Wei, et al. Rapid trajectory optimization for hypersonic entry using convex optimization and pseudospectral method [J]. Aircraft Engineering And Aerospace Technology, 91(4): 669-679, 2019. (SCI 检索)
Changzhu Wei, Yepeng Hanet al. Fifth-Degree Cubature Kalman Filter Estimation of Seeker Line-of-Sight Rate Using Augmented-, Naigang Cui, Dimensional Model [J]. Journal of Guidance, Control, and Dynamics, 40(9): 2355-2362, 2017. (SCI 检索)
Changzhu Wei, Sang-Young Park. Dynamic optimal output feedback control of satellite formation reconfiguration based on an LMI approach[J]. Aerospace Science and Technology, 63: 214-231, 2017. (SCI 检索)
Liang Zhang, Changzhu Wei, Liang Jing, et al. Fixed-time sliding mode attitude tracking control for a submarine-launched missile with multiple disturbances[J]. Nonlinear Dynamics, 93(4): 2543-2563, 2018. (SCI 检索)
Liang Zhang, Changzhu Wei, Rong Wu, et al. Fixed-Time Extended State Observer Based Non-Singular Fast Terminal Sliding Mode Control for a VTVL reusable launch vehicle[J]. Aerospace Science and Technology, 82-83: 70-79, 2018. (SCI 检索)
Rong Wu, Changzhu Wei, Feng Yang, et al. FxTDO-based non-singular terminal sliding mode control for second-order uncertain systems[J]. IET Control Theory and Applications, 12(18): 2459-2467, 2018. (SCI检索)
Feng Yang, Changzhu Wei, Rong Wu, et al. Non-recursive fixed-time convergence observer and extended state observer[J]. IEEE Access, 6: 62339-62351, 2018. (SCI检索)
Panxing Huang, Changzhu Wei, Yuanbei Gu, et al. Hybrid optimization approach for rapid endo-atmospheric ascent trajectory planning[J]. Aircraft Engineering and Aerospace Technology, 88(4): 473-479, 2016. (SCI 检索)
Naiming Qi, Yong Yang, Changzhu Wei, et al. Two-Dimensional Dynamics of a New Configuration of Continuous Cislunar Payloads Transfer System[J]. Transactions of the Japan Society for Aeronautical and Space Sciences, 59(2): 71-80, 2016. (SCI 检索)
Changzhu Wei, Jifeng Guo, Sang-Young Park, et al. IFF Optimal Control for Missile Formation Reconfiguration in Cooperative Engagement[J]. Journal of Aerospace Engineering, 28(3): 04014087, 2015. (SCI 检索)
Changzhu Wei, Sang-Young Park, Chandoek Park. Optimal H-infinity Robust Output Feedback Control for Satellite Formation in Arbitrary Elliptical Reference Orbits[J]. Advanced in Space Research, 54(6), 969-989, 2014. (SCI 检索)
Changzhu Wei, Sang-Young Park, Chandeok Park. Linearized Dynamics Model for Relative Motion under a J(2)-Perturbed Elliptical Reference Orbit[J]. International Journal of Non-Linear Mechanics, 55: 55-69, 2013. (SCI 检索)
Changzhu Wei, Yi Shen, Xiaoxiao Ma, et al. Optimal formation keeping control in missile cooperative Engagement[J]. Aircraft Engineering and Aerospace Technology, 84(6): 376-390, 2012. (SCI 检索)
Naigang Cui, Changzhu Wei, Jifeng Guo, Biao Zhao. Study on Missile Formation Reconfiguration Optimized Trajectory Generation and Control[J]. Journal of Applied Mechanics, 77(5):144-153,2010. (SCI 检索)
EI源及其他：
Naigang Cui, Rong Wu, Changzhu Wei, et al. Double-order power finxed-time convergence sliding mode control method for launch vehicle vertical returning
.Harbin Gongye Daxue Xuebao/Journal of Harbin Institute of Technology, 2020: 15-24. (EI 检索)
Changzhu Wei, Xiaozhe Ju, Dafu Xu, et al. Guidance and control for return process of vertical takeoff vertical landing reusable launching vehicle [C].Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2019: 322782. (EI 检索)
Changzhu Wei, Xiaozhe Ju, Rong Wu, et al. Geometry and time updaters-based arbitrary-yawiterative explicit guidance for fixed-thrust boost back of vertical take-off/vertical landing reusable launch vehicles [C]Aerospace Science and Technology, 2019: 105433. (EI 检索)
Liang Zhang ,Changzhu Wei, Rong Wu, et al. Adaptive fault-tolerant control for a VTVL reusable launch vehicle [C]Acta Astronautica, 2019: 362-370. (EI 检索)
Hao Lee ,Changzhu Wei, et al. A trajectory design method for RLV via artificialmemory-principle optimization [C]MATEC Web of Conferences, 2018: 10019. (EI 检索)
Ruisong Huang ,Hao Lee ,Changzhu Wei, et al. Integrated optimization method of trajectory/system parameters for sub-orbital reusable launch vehicles [C] Zhongguo Guanxing Jishu Xuebao/Journal of Chinese Inertial Technology, 2018: 261-267. (EI 检索)[7]Jinbo Wang ,Naigang Cui ,Changzhu Wei, et al. A Two-stage Rapid Trajectory Optimization Algorithm for Hypersonic Entry [C] IEEE CSAA Guidance, 2018: 9018689. (EI 检索)
Cheng Chen ,Changzhu Wei, Xiaozhe Ju, et al.Robust dynamic inversion control for quad-rotors unmanned vehicle based on sliding mode disturbance observation and compensation [C] Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics, 2018: 119-126. (EI 检索)
Hao Lee, Naigang Cui, Changzhu Wei, et al. Integrated Guidance and Control for Reusable Launch Vehicles with Actuator Failures[C]. 21st AIAA International Space Planes and Hypersonics Technologies Conference, 2017: 2407. (EI 检索)
Changzhu Wei, Xiaozhe Ju, Feiyi He, et al. Research on Non-stationary Control of Advanced Hypersonic Morphing Vehicles[C]. 21st AIAA International Space Planes and Hypersonics Technologies Conference, 2017: 2405. (EI 检索)
Liang Zhang, Rong Wu, Changzhu Wei, et al. Quaternion-Based Reusable Launch Vehicle Composite Attitude Control via Active Disturbance Rejection Control and Sliding Mode Approach[C]. 21st AIAA International Space Planes and Hypersonics Technologies Conference, 2017: 2320. (EI 检索)
Liang Zhang, Changzhu Wei, Liang Jing, Naigang Cui. Heavy Lift Launch Vehicle Technology of Adaptive Augmented Fault Tolerant Control[C]. Proceedings of the 2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC), 2016: 1587-1593 (EI 检索)
Rong Wu, Yingzi Guan, Changzhu Wei, et al. Fixed-Time Disturbance Observer Based Nonsingular Fast Terminal Sliding Mode Guidance with Impact Angle Constraint [C]. Proceedings of the 2018 IEEE/CSAA Guidance, Navigation and Control Conference, Xiamen, China, 2018: 1908-1913. (EI 检索)
Feng Yang, Changzhu Wei, Naigang Cui, Jiangtao Xu. Adaptive generalized super-twisting algorithm based guidance law design. 14th International Workshop on Variable Structure Systems (VSS), 47-52, 2016. (EI 检索)
Chao Cheng, Changzhu Wei, Naigang Cui, Zhiyong She. A measurement method of nonlinear strength for dynamical model of SRLV. International Journal of Modelling, Identification and Control, 24(2): 89-99, 2015. (EI 检索)
Panxing Huang, Changzhu Wei, Yuanbei Gu, Naigang Cui. A symplectic optimisation method for rapid endo-atmospheric ascent trajectory planning. International Journal of Modelling, Identification and Control, 24(3): 196-205, 2015. (EI 检索)
Changzhu Wei, Jifeng Guo, Libin Zhang, Yi Shen, and Naigang Cui. Adaptive Control for Missile Formation Keeping under Leader Information Unavailability. The 10th IEEE International Conference on Control & Automation, Hangzhou, China, 12-14 June 2013: 902-907. (EI 检索)
Naigang Cui, Changzhu Wei, Jifeng Guo and Biao Zhao. Research on Missile Formation Control System. Proceedings of the 2009 IEEE International Conference on Mechatronics and Automation, August 9 – 12. pp: 4197-4202. Changchun, China, 2009. (EI 检索)
Panxing Huang, Yuanbei Gu, Changzhu Wei, Naigang Cui. Reconfigurable Control System Design Based on Control Allocation or HLV. 27th Chinese Control and Decision Conference (CCDC), 3584-3590, 2015.
Naigang Cui, Feng Yang, Changzhu Wei. Three-Dimensional Hit-to-Kill Guidance Law for Direct Thrust Controlled Interceptor. 27th Chinese Control and Decision Conference (CCDC), 4494-4499, 2015.
Changzhu Wei, Naigang Cui, Jifeng Guo. Missiles formation Reconfiguration Optimized trajectory generation and control. The 25th International Symposium on Ballistics, Beijing, China, 2010. No. ISB’10 02-002.
崔乃刚,郭冬子,李坤原,韦常柱.飞行器轨迹优化数值解法综述[J].战术导弹技术,2020(05):37-51+75+5.
崔乃刚,郭冬子,王瑞鸣,王铭泽,韦常柱.飞航导弹智能故障诊断与容错控制[J].战术导弹技术,2020(04):125-134.
崔乃刚,吴荣,韦常柱,徐大富.火箭垂直返回双幂次固定时间收敛滑模控制方法[J].哈尔滨工业大学学报,2020,52(04):15-24.
韦常柱,琚啸哲,何飞毅,潘豪,徐世昊.运载火箭主动段自适应增广控制[J].宇航学报,2019,40(08):918-927.
韦常柱,琚啸哲,徐大富,吴荣,崔乃刚.垂直起降重复使用运载器返回制导与控制[J].航空学报,2019,40(07):197-220.
邵会兵,崔乃刚,韦常柱.滑翔导弹末段多约束智能弹道规划[J].光学精密工程,2019,27(02):410-420.
徐世昊,崔乃刚,韦常柱.基于RBF神经网络的导弹智能控制系统设计[J].宇航总体技术,2018,2(06):19-26.
高兴,张璐,韦常柱.面向禁飞区约束的再入滑翔飞行器快速轨迹规划[J].战术导弹技术,2018(05):62-67+94.
杨峰, 韦常柱, 吴荣, 等. 一阶不确定系统的固定时间收敛扰动观测器[J]. 控制与决策. (published online, EI 检索)
韦常柱, 琚啸哲, 何飞毅, 等. 运载火箭主动段自适应增广控制研究[J]. 宇航学报. (published online, EI检索)
陈诚, 韦常柱, 琚啸哲, 等. 基于滑模观测补偿的四旋翼飞行器鲁棒动态逆控制[J]. 系统工程与电子技术, 2018, 40(1): 119-126. (EI 检索)
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崔乃刚, 黄盘兴, 路菲, 黄荣, 韦常柱. 基于混合优化的运载器大气层内上升段轨迹快速规划方法[J]. 航空学报, 2015, 36(6): 1915-1923. (EI 检索)
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黄荣, 崔乃刚, 韦常柱, 等. 基于 RRT-GPM 两阶策略的导弹编队协同突防最优轨迹快速设计[J]. 中国惯性技术学报, 2015, 23(3): 356-362. (EI 检索)
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韦常柱, 郭继峰, 崔乃刚. 导弹协同作战编队队形最优保持控制器设计[J]. 宇航学报, 2010, 31(4): 1043-1050. (EI 检索)
韦常柱, 郭继峰, 赵彪. 导弹协同作战编队飞行控制系统研究[J]. 系统工程与电子技术, 2010, 32(9): 1968-1972. (EI 检索)
浦甲伦, 韦常柱, 荣思远. 修正增益卡尔曼滤波算法在被动测距问题中的应用[J]. 宇航学报, 2008, 28(4): 886-889. (EI 检索)
许江涛, 崔乃刚, 路菲, 韦常柱. 无人机非方阵系统解耦控制[J]. 航空学报, 2008, 29(5): 157-162. (EI 检索)
韦常柱, 张立佳, 崔乃刚. 布撒器对机场跑道的封锁方式及概率分析[J]. 弹道学报, 2008, 20(2): 32-36. (EI 检索)
张亮, 黄盘兴, 徐大富, 韦常柱, 黄荣. 垂直起降火箭垂直返回段自适应容错控制算法[J]. 战术导弹技术, 2015 (2): 63-69.
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专著
Changzhu Wei, Yi Shen, Naigang Cui, Sang-Young Park and Jifeng Guo. Chapter 11: Missile Cooperative Engagement Formation Configuration Control Method. In "Recent Advances in Robust Control – Theory and Applications in Robotics and Electromechanics", INTECH Open Access Publisher, 2012, ISBN 978-953-307-421-4.
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