Tian Bailing, Yin Liping and Wang Hong. Finite Time Reentry Attitude Control Based on Adaptive Multivariable Disturbance Compensation. IEEE Transaction on Industrial Electronics, 62(9): 5889-5898, 2015.
Tian Bailing, Fan Wenru and Qun Zong. Real-Time Trajectory and Attitude Coordination Control for Reusable Launch Vehicle in Reentry Phase. IEEE Transaction on Industrial Electronics, 62(3):1639-1650,2015.
 Tian Bailing, Fan Wenru,Qun Zong.Integrated Guidance and Control for Reusable Launch Vehicle in Reentry Phase. Nonlinear Dynamics 80(1-2):397-412,2015.
 Tian Bailing, Yan Xiaomo, Wang Hong. Fault-Tolerant Control Scheme For Manipulator with Actuator and Sensor Failure. International Journal of Advanced Mechatronic Systems, 64(6):166-173,2015.
 Bailing Tian, Wenru Fan, Rui Su, and Qun Zong. Nonlinear Robust Adaptive Deterministic Control for Flexible Hypersonic Vehicles in the Presence of Input Constraint, Asian Journal of Control, 17(6): 2303–2316,2015.
Bailing Tian, Wenru Fan, Qun Zong, Jie Wang, Fang Wang.Nonlinear robust control for reusable launch vehicles in reentry phase based on time-varying high order sliding mode.Journal of the Franklin Institute,380(7):1787-1807, 2013.
 Tian Bailing, Su Rui, Fan Wenru. Multiple Time Scale Smooth Second Order Sliding Mode Controller Design for Flexible Hypersonic Vehicles.Journal of Aerospace Engineering 229(5):781-791,2015.
 Bailing Tian, Qun Zong, Jie Wang, Fang Wang. Quasi-continuous high-order sliding mode controller design for reusable launch vehicles in reentry phase, Aerospace Science and Technology,28(1):198-207,2013.
 Bailing Tian, Wenru Fan, Qun Zong, Jie Wang, Fang Wang. Adaptive High Order Sliding Mode Controller Design for Hypersonic Vehicle with Flexible Body Dynamics. Mathematical Problems in Engineering,2013.
 Tian Bailing, Qun Zong. Optimal Guidance for Reentry Vehicles Based on Indirect Legendre Pseudospectral Method. Acta Astronautica. 2011, 68(7-8):1176-1184.
 Qun Zong, Tian Bailing, Liqian Dou, Chaofang Hu. Ascent Phase Trajectory Optimization for Vehicle with Space Restricted. Transactions of the Japan Society for Aeronautical and Space Sciences. 2011, 54(183):37-43.
 宗群，田栢苓。基于Gauss伪谱法的临近空间飞行器上升段轨迹优化。宇航学报, 31(7):1775-1781, 2010.
Xiaomo Yan, Bailing Tian and Hong Wang. An adaptive observer-based fault detection and diagnosis for nonlinear systems with sensor and actuator faults. 2015 International Conference on Advanced Mechatronic Systems,491-496,2015.
 Qun Zong, Tian Bailing. Quasi-Continuous High-Order Sliding Mode Controller and Observer Design for Hypersonic Vehicle. 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, San Francisco, USA. (AIAA-2011-2384).
 Tian Bailing, Qun Zong. Ascent Phase Trajectory Optimization for Aircraft Based on Nonlinear Programming. The 22nd Chinese Control and Decision Conference, Xu Zhou, China, pp.2076-2081. 2010. (EI: 20103213140193).
 Tian Bailing, Qun Zong. Smooth Second Order Sliding Mode Control for RLV in Reentry Phase, Control Conference (CCC), 2012 31st Chinese, Hefei, China, pp.583–588, 2012.
 Tian Bailing, Qun Zong. 3DOF Ascent Phase Trajectory Optimization Based on Adaptive Gauss Method, Intelligent Control and Information Processing (ICICIP), 2012 Third International Conference on, Dalian, China,pp. 431-435,2012.
 Bailing Tian, Wenru Fan. Adaptive High Order Sliding Mode Controller Design for Hypersonic Vehicle, The 10th IEEE International Conference on Control & Automation, Hangzhou,China, 2013,pp.464-468.