Yan J, Zhang J, Liu P, et al. A new IFNTSM controller design for the BWB aircraft with parameter uncertainties[C]// Chinese Automation Congress. 2017:6167-6171.
Xu Y, Zhang J, Yang L, et al. Integrated flight/propulsion optimal control for DPC aircraft based on the BO-PSO algorithm[C]// Chinese Control Conference. 2017:11453-11458.
Xie Q, Yang L, Yang X. Micro Aerial Vehicle Indoor Localization using Prior Map and Spare Sonars[C]// 中国控制会议. 2017:5534-5538.
Zhou H, Yang L, Zhang J, et al. Online learning and inference based flight envelope estimation for aircraft loss-of-control prevention[C]// IEEE International Conference on Control & Automation. IEEE, 2017:100-106.
Yang X, Yang L, Zhang J. A WiFi-enabled indoor air quality monitoring and control system: The design and control experiments[C]// IEEE International Conference on Control & Automation. IEEE, 2017:927-932.
Yan J, Zhang J, Li H. Design of aircraft center of gravity control law based on sliding mode control[C]// IEEE International Conference on Aircraft Utility Systems. IEEE, 2016:438-442.
Yang X, Luo M, Zhang J, et al. Aircraft centre-of-gravity estimation using Gaussian process regression models[C]// IEEE International Conference on Aircraft Utility Systems. IEEE, 2016:991-995.
Peng B, Yang L, Yang X. LPV-MRAC Method for Aircraft with Structural Damage[C]// Control Conference. IEEE, 2016:3262-3267.
Yang X, Peng B, Zhou H, et al. State estimation for nonlinear dynamic systems using Gaussian processes and pre-computed local linear models[C]// Guidance, Navigation and Control Conference. IEEE, 2017:1963-1968.
Zhang J, Zeng X, Yang L. Analysis of coupling effects between flight and propulsion systems for DPC aircraft[C]// World Congress on Intelligent Control and Automation. 2016:1653-1657.
Peng J, Jing Z, Yang L. Adaptive non-singular terminal sliding mode control for structural damaged aircraft[C]// Control Conference. IEEE, 2015:716-720.
Hu X, Yang L, Zhang J. The design and analysis of hierarchical decision-making for manned/unmanned cooperative engagement[C]// Control Conference. Technical Committee on Control Theory, Chinese Association of Automation, 2015:2698-2703.
Kang W, Zhang J, Yang L. Research on Boundary Layer Ingestion effects of distributed propulsion configuration[C]// Guidance, Navigation and Control Conference. IEEE, 2015:624-629.
Kang W, Zhang J, Yang L. Research on supercirculation effects of distributed propulsion configuration[C]// Guidance, Navigation and Control Conference. IEEE, 2014:720-725.
康文文, 朱亮. 基于云知识管理平台的IPT模式及民机研制系统集成能力建设[C]// 2014中国制导、导航与控制学术会议. 2014.
朱亮, 康文文. 复杂产品研发过程中的技术评审与审核问题初探[C]// 2014中国制导、导航与控制学术会议. 2014.
Xu X, Yang L, Hu X, et al. Mission-oriented control scheme for autonomous/semi-autonomous UCAV[C]// Guidance, Navigation and Control Conference. IEEE, 2015:2734-2739.
He C, Yang L, Wang Z, et al. Linear Parameter-Varying Attitude Controller Design for a Reusable Launch Vehicle during Reentry[C]// 2014中国制导、导航与控制学术会议. 2014:2723-2728.
Li A, Yang L, Zhang J, et al. LQR and Fuzzy Gain-Scheduling based attitude controller for RLV within large operating envelope[C]// IEEE International Conference on Control Science and Systems Engineering. IEEE, 2015:51-56.
Wang Y, Yang L, Zhang J, et al. An observer based multivariable adaptive reconfigurable control method for the wing damaged aircraft[C]// IEEE International Conference on Control & Automation. IEEE, 2014:95-100.
Wang Z, Yang L, Zhang J, et al. Integer programming based optimal side jets ignition combination for advanced missile attitude control[C]// Control and Decision Conference. IEEE, 2014:3755-3759.
何超凡, 杨凌宇, 张晶. 高超声速飞行器模型预测控制器设计方法研究[C]// the 32nd chinese control conference. 2013.
韩婵, 杨凌宇, 张晶. 面向重心变化的预估模型参考自适应控制器设计[C]// the 32nd chinese control conference. 2013.
Zhang G, Yang L, Zhang J, et al. Longitudinal attitude controller design for aircraft landing with disturbance using ADRC/LQR[C]// IEEE International Conference on Automation Science and Engineering. IEEE, 2013:330-335.
Wang Y, Yang L, Zhang J, et al. A multivariable adaptive reconfigurable control method applied to the wing damaged aircraft[C]// IEEE International Conference on Control and Automation. IEEE, 2013:1828-1833.
韩婵, 杨凌宇. 结构受损飞机建模、动力学特性分析与仿真[C]// 2012中国制导、导航与控制学术会议
邹景锋，杨凌宇，张晶，申功璋. 鲁棒控制分配方法研究及其鲁棒性评估[C]//2012中国制导、导航与控制学术会议
魏和平，杨凌宇，张晶，申功璋. 空战战机导引决策研究[C]// 2012中国制导、导航与控制学术会议
冷宁，杨凌宇，申功璋. 非对称结构受损飞机多变量模型参考自适应飞行控制研究[C]// 2012中国制导、导航与控制学术会议
何超凡, 杨凌宇, 申功璋, 张晶. 基于间隙度量的高超声速飞行器包线划分方法研究[C]// 2012中国制导、导航与控制学术会议
Zou J, Yang L, Zhang J, et al. Research on robust control allocation for the advanced configuration aircraft[C]// Intelligent Control and Automation. IEEE, 2012:1722-1726.
Yinan L, Lingyu Y, Gongzhang S. Steady maneuver envelope evaluation for aircraft with control surface failures[C]// 2012:1-10.
唐志帅，杨凌宇，张晶，申功璋. 大型飞机推力调节（PCA）鲁棒控制器设计[C]// 第三届信息、电子与计算机工程国际学术会议(ICIECS 2011).
Ergang Chen, Lingyu Yang, Gongzhang Shen. The aircraft cabin system simulation based on GL Studio[C]// 2011 3rd International Conference on Information, Electronic and Computer Science
Han J, Yang L, Zhang Z, et al. Predictor-corrector guidance based on optimization[C]// International Conference on Electronics, Communications and Control. IEEE, 2011:2757-2761.
Wen Y, Yang L, Shen G. Aerodynamic characteristics analysis and capability assessment of structural damaged aircraft with advanced configuration[C]// International Conference on Electronics, Communications and Control. IEEE, 2011:2506-2511.
高博，杨凌宇，申功璋. 基于结构奇异值的鲁棒特征结构配置及应用[C]// 2010中国制导、导航与控制学术会议.
张增辉，杨凌宇，申功璋. 可重复使用运载器初始再入段轨迹规划[C]// 2010中国制导、导航与控制学术会议.
边一齐,杨凌宇, 赵佳, 申功璋. 直升机时变参考模型自适应逆姿态控制研究[C]// 2010年中国导航制导与控制学术会议.
温阳，李亦楠，杨凌宇. 前下视景象匹配关键技术研究与仿真[C]// 2010中国制导、导航与控制学术会议.
张晶，申功璋，杨凌宇. 面向重心变化的自适应飞行控制系统设计[C]// 2010中国制导、导航与控制学术会议.
郭元江，杨汀，李会杰，景海峰，张晶，杨凌宇，申功璋. 复杂环境下舰载机弹射起飞环境因素建模分析 [C]// 2010中国制导、导航与控制学术会议.
赵佳, 申功璋. 直升机旋转逆动力学建模及姿态控制研究[J]. 电机与控制学报, 2010, 14(8):31-37.
Zhang Z, Yang L, Zhong Y, et al. Modeling and analysis for a generic hypersonic vehicle[C]// Intelligent Control and Automation. 2010:152-158.
杨凌宇, 齐万强, 钟友武,等. 基于力矩补偿与分配的多操纵面飞机飞行控制设计[C]// 中国航空学会控制与应用学术年会. 2008.
