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近年学术论文(英文)
[2022] Yudong Hu, Changsheng Gao,Junlong Li, Wuxing Jing,Wenxue Chen .A novel adaptive lateral reentry guidance algorithm with complex distributed no-fly zones constraints. Chinese Journal of Aeronautics.2022
[2022]Xiaoqi Qiu, Changsheng Gao, Kefan Wang, Wuxing Jing. Attitude control of a moving-mass actuated UAV based on deep reinforcement learning. Journal of Aerospace Engineering. 2022: 35(2)
[2022]Xiaoqi Qiu, Changsheng Gao, Wuxing Jing .Maneuvering Penetration Strategies of Ballistic Missiles Based on Deep Reinforcement Learning. IMechE Part G: Journal of Aerospace Engineering.2022
[2022] Peng Cui, Changsheng Gao.Neural Sliding Mode Tracking Control of Air-breathing Hypersonic Vehicles. Journal of Physics: Conference Series (JPCS). 2022.4
[2022] Jiahui Sun, Wuxing Jing, Changsheng Gao, Tong Wu .Attitude dynamics and control of high-mass-ratio fixed-trim moving mass reentry vehicle. Aerospace Science and Technology. 2022,123
[2022] Yiting Tan，Wuxing Jing, Changsheng Gao. Uncertain trajectory planning integrating polynomial chaos and convex programming. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 2022，3
[2021] Yudong Hu, Changsheng Gao,Junlong Li, Wuxing Jing.Maneuver mode analysis and parametric modeling for hypersonic glide vehicles. Aerospace Science and Technology. 2021, 119C
[2021] Yudong Hu, Changsheng Gao,Junlong Li, Wuxing Jing.Novel trajectory prediction algorithms for hypersonic gliding vehicles based on maneuver mode on-line identification and intent inference. Measurement Science and Technology. 2021, 32(11)
[2021] Yiting Tan，Wuxing Jing, Changsheng Gao. Stochastic Trajectory Planning Considering Parameter and Initial State Uncertainties.2021 China Automation Congress.2021
[2021] Guanghui ChengWuxing Jing, Changsheng Gao.Recovery trajectory planning for the reusable launch vehicle. Aerospace Science and Technology. 2021(117)
[2021] Biao Yang, Wuxing Jing, Changsheng Gao. Online midcourse guidance method for boost phase interception via adaptive convex programming. Aerospace Science and Technology. 2021, 118: 107037
[2021] Yidi Fan, Wuxing Jing, Changsheng Gao, Franco Bernelli-Zazzera . Immersion and invariance-based adaptive coordinate control for space manipulator. 021 IEEE 7th International Conference on Control Science and Systems Engineering (ICCSSE).
[2021] Qiu X , Zhang M , Jing W , et al. Dynamics and Adaptive Sliding Mode Control of a Mass-Actuated Fixed-Wing UAV[J]. International Journal of Aeronautical and Space Sciences, 2021:1-12.
[2021] Feng Gao,Wei Zhong,Zhigang Li, Wuxing Jing, Changsheng Gao.A Pose Synchronization Control Method for the Approach Phase of Lunar Lander. 2021 China Automation Congress (CAC)
[2020] Yang Biao, Jing Wuxing, Gao Changsheng. Three-dimensional cooperative guidance law for multiple missiles with impact angle constraint. Journal of Systems Engineering and Electronics. 2020, 31(6):1286-1296
[2020] Biao Yang, Wuxing Jing, Changsheng Gao. Design of midcourse trajectory for boost phase interception. 2020 International Conference on Guidance, Navigation and Control, Tianjin, China. 2020
[2020] Zhao Zhang, Wuxing Jing, Changsheng Gao. Improvementof ensemble Kalman filter for hypersonic target tracking. Journal of Electronic Imaging. 2020
[2019] Wei P , Gao C , Jing W . Longitudinal Aerodynamic Coefficients Estimation and Identifiability Analysis for Hypersonic Glider Controlled by Moving Mass[J]. International Journal of Aeronautical & Space Sciences, 2019.
[2019] Jiang C , Zhou G , Gao C , et al. Nonlinear reentry guidance law guaranteeing convergence before attainment of desired line-of-sight range[J]. Aerospace Science and Technology, 2019, 92(SEP.):579-587.
[2019] Zheng X , Jing W , Gao C . Trajectory characteristic analysis influenced by initial state errors for long-range vehicles[J]. Proceedings of the Institution of Mechanical Engineers, 2019, 233(7):2413-2432.
[2019] Zheng X , Jing W , Gao C . Influence of Initial State Errors on Perturbation Guidance Accuracy[J]. Defence Science Journal, 2019, 69(1):10-19.
[2019] Chen E , Jing W , Gao C . Sensor placement and moving horizon state/parameter estimation for flexible hypersonic vehicles[J]. Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering, 2019.
[2019] Wei P , Jing W , Gao C . Dynamics and Control for Hypersonic Gliding Vehicles Equipped with a Moving Mass and RCS[J]. Journal of Aerospace Engineering, 2019, 32(5).
近年学术论文(中文)
[2022] 邱潇颀,高长生,荆武兴.拦截大气层内机动目标的深度强化学习制导律. 宇航学报.
[2021]高长生,王越欣,荆武兴,胡玉东.一种高超声速飞行器在线反馈滤波算法[J].现代防御技术,2021,49(01):1-7.
[2021]邱潇颀,高长生,荆武兴.变质心固定翼无人机动力学分析与抗扰控制[J/OL].北京航空航天大学学报: 2021，1-12[.
[2021]刘智陶,李涧青,高长生.欠驱动变质心飞行器的滚偏耦合自抗扰控制[J].北京航空航天大学学报,2021,47(02):281-288.
[2021] 荆武兴, 杨彪, 高长生. 空基反助推段导弹制导技术综述. 哈尔滨工业大学学报. 2021, 53(06): 1-12
[2021] 谭一廷，荆武兴,高长生. 考虑零控交班视窗角约束的拦截中制导设计. 宇航学报. 2021，42（10）
[2021] 高峰 ,荆武兴 ,高长生 ,李志刚 ,钟伟. 经济型月球探测器精确定点软着陆制导算法. 宇航学报. 2021,42(10)
[2020]杨彪,荆武兴,李涧青,高长生.动能拦截器运动伪装末制导律设计[J].宇航学报,2020,41(01):91-100.
[2019]陈尔康,荆武兴,高长生.弹性高超声速滑翔飞行器的状态/参数联合估计[J].航空学报,2019,40(08):248-259.
[2019]张召,荆武兴,李君龙,高长生.谱估计理论在弹道数据参数化建模中的应用[J].宇航学报,2019,40(12):1453-1460.
[2019]李臻,杨彪,荆武兴,高长生,常武权.逃逸飞行器轨迹鲁棒性快速评估及制导[J].载人航天,2019,25(06):699-708.
[2019]陈尔康,荆武兴,高长生.弹性高速飞行器的状态/参数滚动时域估计[J].北京航空航天大学学报,2019,45(02):291-298.
[2019]张召,王恒,荆武兴,高长生.大气层外多拦截器协同跟踪与制导算法[J].宇航学报,2019,40(07):785-793.
[2019]范一迪,荆武兴,高长生,杜华军.滚控式变质心飞行器动力学特性分析与控制[J].宇航学报,2019,40(04):386-395.
[2019]陈尔康,高长生,荆武兴.空间目标的轨迹和姿态数据生成[J].西北工业大学学报,2019,37(02):378-385.
轨迹估计预报方面部分学术论文
[2021] Yudong Hu, Changsheng Gao,Junlong Li, Wuxing Jing.Maneuver mode analysis and parametric modeling for hypersonic glide vehicles. Aerospace Science and Technology. 2021, 119C
[2021] Yudong Hu, Changsheng Gao,Junlong Li, Wuxing Jing.Novel trajectory prediction algorithms for hypersonic gliding vehicles based on maneuver mode on-line identification and intent inference. Measurement Science and Technology. 2021, 32(11)
[2020] Zhao Zhang, Wuxing Jing, Changsheng Gao. Improvementof ensemble Kalman filter for hypersonic target tracking. Journal of Electronic Imaging. 2020
[2019] Wei P , Gao C , Jing W . Longitudinal Aerodynamic Coefficients Estimation and Identifiability Analysis for Hypersonic Glider Controlled by Moving Mass[J]. International Journal of Aeronautical & Space Sciences, 2019.
[2019] Chen E , Jing W , Gao C . Sensor placement and moving horizon state/parameter estimation for flexible hypersonic vehicles[J]. Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering, 2019.
[2018]Zhang, Zhao, Gao C, et al. Infrared measurement and composite tracking algorithm for air-breathing hypersonic vehicles[J]. Journal of Electronic Imaging, 2018.
[2016]Jianqing Li,Changsheng Gao,Tianming Feng,Wuxing Jing. Error Correction of Infrared Earth Radiance for Autonomous Navigation[J]. The Journal of Navigation,2016,69(6).
[2021]高长生,王越欣,荆武兴,胡玉东.一种高超声速飞行器在线反馈滤波算法[J].现代防御技术,2021,49(01):1-7.
[2019]陈尔康,荆武兴,高长生.弹性高超声速滑翔飞行器的状态/参数联合估计[J].航空学报,2019,40(08):248-259.
[2019]陈尔康,高长生,荆武兴.空间目标的轨迹和姿态数据生成[J].西北工业大学学报,2019,37(02):378-385.
[2019]张召,荆武兴,李君龙,高长生.谱估计理论在弹道数据参数化建模中的应用[J].宇航学报,2019,40(12):1453-1460.
[2019]陈尔康,荆武兴,高长生.弹性高速飞行器的状态/参数滚动时域估计[J].北京航空航天大学学报,2019,45(02):291-298.
[2017]封天明,李涧青,高长生,荆武兴.考虑地球敏感器误差的自主导航方法研究[J].上海航天,2017,34(02):112-119.
[2016]郑旭,高长生,荆武兴,常晓华.发射初态误差对弹道特征参数的影响[J].固体火箭技术,2016,39(03):436-443.
[2010]钱霙婧,荆武兴,高长生.多航天器部署问题中的自主导航方法研究[J].哈尔滨工业大学学报,2010,42(05):705-709.
宽域飞行制导方面部分学术论文
[2022] Yudong Hu, Changsheng Gao,Junlong Li, Wuxing Jing ，Wenxue Chen.A novel adaptive lateral reentry guidance algorithm with complex distributed no-fly zones constraints. Chinese Journal of Aeronautics.2022
[2021] Biao Yang, Wuxing Jing, Changsheng Gao. Online midcourse guidance method for boost phase interception via adaptive convex programming. Aerospace Science and Technology. 2021, 118: 107037
[2020] Yang Biao, Jing Wuxing, Gao Changsheng. Three-dimensional cooperative guidance law for multiple missiles with impact angle constraint. Journal of Systems Engineering and Electronics. 2020, 31(6):1286-1296
[2020] Biao Yang, Wuxing Jing, Changsheng Gao. Design of midcourse trajectory for boost phase interception. 2020 International Conference on Guidance, Navigation and Control, Tianjin, China. 2020
[2020] X Zheng, Gao C , Jing W , et al. Multidisciplinary integrated design of long-range ballistic missile using PSO algorithm[J]. Journal of Systems Engineering and Electronics, 2020, 31(2):335-349.
[2019] Jiang C , Zhou G , Gao C , et al. Nonlinear reentry guidance law guaranteeing convergence before attainment of desired line-of-sight range[J]. Aerospace Science and Technology, 2019, 92(SEP.):579-587.
[2019] Zheng X , Jing W , Gao C . Influence of Initial State Errors on Perturbation Guidance Accuracy[J]. Defence Science Journal, 2019, 69(1):10-19.
[2018]C. Gao,J. Li,T. Feng,W. Jing. Adaptive terminal guidance law with impact-angle constraint[J]. The Aeronautical Journal,2018,122(1249).
[2017] Changsheng Gao, Jianqing Li, Huajun Du,Wuxing Jing,Guidance Method for Braking Phase of Lunar Lander, Journal of Spacecraft and Rockets,2017,54(2):523-528
[2016]Chang-sheng Gao,Jian-qing Li,Wu-xing Jing,Christopher J. Damaren. A Terminal Guidance Law Based on Motion Camouflage Strategy of Air-to-Ground Missiles[J]. International Journal of Aerospace Engineering,2016,2016.
[2016] Erkang Chen，Wuxing Jin, Changsheng Gao. Virtual Displacement Guidance for Hypersonic Glide Vehicle. 35th Chinese Control Conference.2016
[2022] 邱潇颀,高长生,荆武兴.拦截大气层内机动目标的深度强化学习制导律. 宇航学报. 2022
[2021] 谭一廷，荆武兴,高长生. 考虑零控交班视窗角约束的拦截中制导设计. 宇航学报. 2021，42（10）
[2021] 荆武兴, 杨彪, 高长生. 空基反助推段导弹制导技术综述. 哈尔滨工业大学学报. 2021, 53(06): 1-12
[2020]杨彪,荆武兴,李涧青,高长生.动能拦截器运动伪装末制导律设计[J].宇航学报,2020,41(01):91-100.
[2019]李臻,杨彪,荆武兴,高长生,常武权.逃逸飞行器轨迹鲁棒性快速评估及制导[J].载人航天,2019,25(06):699-708.
[2019]张召,王恒,荆武兴,高长生.大气层外多拦截器协同跟踪与制导算法[J].宇航学报,2019,40(07):785-793.
[2016]高长生，李涧青，荆武兴，拦截机动目标的运动伪装制导律，宇航学报，37（6）：736-742，2016.
[2016]郑旭,高长生,陈尔康,荆武兴.一种基于大气层外解析动力学模型的最优迭代制导方法[J].西北工业大学学报,2016,34(06):1093-1100.
[2013]魏鹏鑫,荆武兴,高长生.具有落角约束的弹道导弹再入末制导律设计[J].哈尔滨工业大学学报,2013,45(09):23-30.
[2012]韦文书,荆武兴,高长生.机动发射的弹道导弹飞行诸元的快速计算[J].哈尔滨工业大学学报,2012,44(11):7-12.
[2009]高长生,李瑞康,荆武兴.新型制导律在变质心再入飞行器中的应用[J].哈尔滨工业大学学报,2009,41(03):6-10.
[2007]高长生,荆武兴,郑立伟.再入弹道解析算法在新型制导律上的应用研究[J].宇航学报,2007(05):1219-1223.
轨迹规划与博弈对抗方面部分学术论文
[2022]Xiaoqi Qiu, Changsheng Gao, Wuxing Jing .Maneuvering Penetration Strategies of Ballistic Missiles Based on Deep Reinforcement Learning. IMechE Part G: Journal of Aerospace Engineering.2022
[2022] Yiting Tan，Wuxing Jing, Changsheng Gao. Uncertain trajectory planning integrating polynomial chaos and convex programming. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 2022，3
[2021] Yiting Tan，Wuxing Jing, Changsheng Gao. Stochastic Trajectory Planning Considering Parameter and Initial State Uncertainties.2021 China Automation Congress.2021
[2021] Guanghui Cheng,Wuxing Jing, Changsheng Gao.Recovery trajectory planning for the reusable launch vehicle. Aerospace Science and Technology. 2021(117)
[2019] Zheng X , Jing W , Gao C . Trajectory characteristic analysis influenced by initial state errors for long-range vehicles[J]. Proceedings of the Institution of Mechanical Engineers, 2019, 233(7):2413-2432.
[2018]Z. Zhang, C. Gao, W. Jing and E. Chen, "Firing Data Design for the Midcourse Interceptor with Complex Flight Program," 2018 9th International Conference on Mechanical and Aerospace Engineering (ICMAE), Budapest, 2018, pp. 190-198. doi: 10.1109/ICMAE.2018.8467690
[2017] Gao C , Jiang C , Jing W , et al. Optimization of projectile state and trajectory of reentry body considering attainment of carrying aircraft[J]. Journal of Systems Engineering and Electronics, 2017.
[2017]高长生,陈尔康,荆武兴.高超声速飞行器机动规避轨迹优化[J].哈尔滨工业大学学报,2017,49(04):16-21.
大气飞行器姿态控制方面部分学术论文(英文)
[2022]Xiaoqi Qiu, Changsheng Gao, Kefan Wang, Wuxing Jing. Attitude control of a moving-mass actuated UAV based on deep reinforcement learning. Journal of Aerospace Engineering. 2022: 35(2)
[2022] Peng Cui, Changsheng Gao.Neural Sliding Mode Tracking Control of Air-breathing Hypersonic Vehicles. Journal of Physics: Conference Series (JPCS). 2022.4
[2022] Jiahui Sun, Wuxing Jing, Changsheng Gao, Tong Wu .Attitude dynamics and control of high-mass-ratio fixed-trim moving mass reentry vehicle. Aerospace Science and Technology. 2022,123
[2021] Yidi Fan, Wuxing Jing, Changsheng Gao, Franco Bernelli-Zazzera . Immersion and invariance-based adaptive coordinate control for space manipulator. 021 IEEE 7th International Conference on Control Science and Systems Engineering (ICCSSE).
[2019] Wei P , Jing W , Gao C . Dynamics and Control for Hypersonic Gliding Vehicles Equipped with a Moving Mass and RCS[J]. Journal of Aerospace Engineering, 2019, 32(5).
[2018]E. Chen, W. Jing, C. Gao and Z. Zhang, "An Adaptive Control Approach for a Flexible Hypersonic Glide Vehicle," 2018 9th International Conference on Mechanical and Aerospace Engineering (ICMAE), Budapest, Hungary, 2018, pp. 1-5. doi: 10.1109/ICMAE.2018.8467711
[2018] Gao C , Li J , Fan Y , et al. Immersion and invariance-based control of novel moving-mass flight vehicles[J]. Aerospace Science and Technology, 2018, 74(MAR.):63-71.
[2018]J. Li, S. Chen, C. Li, C. Gao and M. Yu, "ADRC-based Longitudinal Control for Novel Flight Vehicle with Moving Mass," 2018 IEEE Conference on Decision and Control (CDC), Miami, FL, USA, 2018, pp. 601-606. doi: 10.1109/CDC.2018.8619799
[2018] Li J , Gao C , Li C , et al. A survey on moving mass control technology[J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 82-83(NOV.):594-606.
[2018] Liu Z , Gao C , Li J , et al. Closed-Loop Bifurcation Analysis for a Novel Moving Mass Flight Vehicle[J]. International Journal of Aeronautical and Space Sciences, 2018, 19(4):962-975.
[2018]ChangshengGao, JianqingLi, YidiFan？, WuxingJing，Research on Application of Single Moving Mass in the Reentry Warhead Maneuver，Aerospace Science and Technology，74：63-71，2018
[2017]Jianqing Li,Changsheng Gao,Wuxing Jing,Pengxin Wei. Dynamic analysis and control of novel moving mass flight vehicle[J]. Acta Astronautica,2017,131.
[2016]Changsheng Gao,Chunwang Jiang,Yan Zhang,Wuxing Jing,Kenneth M. Sobel. Three-Dimensional Integrated Guidance and Control for Near Space Interceptor Based on Robust Adaptive Backstepping Approach[J]. International Journal of Aerospace Engineering,2016,2016.
大气飞行器姿态控制方面部分学术论文(中文)
[2021]邱潇颀,高长生,荆武兴.变质心固定翼无人机动力学分析与抗扰控制[J/OL].北京航空航天大学学报:1-12[2021-04-01].
[2021]刘智陶,李涧青,高长生.欠驱动变质心飞行器的滚偏耦合自抗扰控制[J].北京航空航天大学学报,2021,47(02):281-288.
[2019]范一迪,荆武兴,高长生,杜华军.滚控式变质心飞行器动力学特性分析与控制[J].宇航学报,2019,40(04):386-395.
[2017]李涧青,高长生,荆武兴. 单滑块变质心飞行器动力学与控制问题[A]. 中国力学学会动力学与控制专业委员会多体动力学与控制专业组研讨会,2017:1.
[2016]李涧青,高长生,荆武兴,杜华军.俯控式单滑块变质心飞行器控制问题[J].中国科学:技术科学,2016,46(10):1048-1056.
[2013]高长生,张研,魏鹏鑫,荆武兴.质量矩控制自旋弹弹体性能分析[J].飞行力学,2013,31(01):61-64.
[2012]魏鹏鑫,高长生,荆武兴.质量矩控制飞行器的压心不确定性问题研究[J].航天控制,2012,30(02):39-45.
[2011]高长生,荆武兴,李君龙.基于自适应反演法的质量矩导弹控制律设计[J].兵工学报,2011,32(06):686-690.
[2011]魏鹏鑫,高长生,荆武兴.基于自适应滑模的变质心再入飞行器控制律设计[J].上海航天,2011,28(05):1-7.
[2010]高长生,荆武兴,于本水,李君龙.质量矩导弹构型及自适应控制律设计[J].航空学报,2010,31(08):1593-1599.
[2010]高长生,李君龙,荆武兴,李瑞康.导弹质量矩控制技术发展综述[J].宇航学报,2010,31(02):307-314.
[2010]李瑞康,高长生,荆武兴,钱霙婧.飞行器变质心控制及性能分析[J].宇航学报,2010,31(09):2165-2171.
[2010]李瑞康,荆武兴,高长生,杜华军.基于布局优化的飞行器变质心控制性能研究[J].上海航天,2010,27(01):9-14.
[2009]李瑞康,荆武兴,高长生,杜华军.再入弹头质量矩复合控制系统设计[J].航天控制,2009,27(04):43-48+52.
航天器轨道姿态方面部分学术论文
[2021] 高峰 ,荆武兴 ,高长生 ,李志刚 ,钟伟. 经济型月球探测器精确定点软着陆制导算法. 宇航学报. 2021,42(10)
[2017]罗绪盛,荆武兴,高长生.火星探测捕获的误差传播分析[J].系统工程与电子技术,2017,39(07):1590-1595.
[2014]李涧青,高长生,郑建华,荆武兴.基于金星借力的黄道面外日冕探测器轨道设计[J].上海航天,2014,31(06):22-25+72.
[2013]韦文书,荆武兴,高长生.捕获非合作目标后航天器的自主稳定技术研究[J].航空学报,2013,34(07):1520-1530.
[2013]钱霙婧,荆武兴,高长生,韦文书.地月平动点拟周期轨道探测器自主导航方法研究[J].宇航学报,2013,34(05):625-633.
[2012]魏鹏鑫,荆武兴,高长生.轨道要素奇异问题的改进四元数方法[J].中国空间科学技术,2012,32(01):66-71.
[2007]高长生,荆武兴.同地迹八颗IGSO卫星区域导航星座分析[J].哈尔滨工业大学学报,2007(07):1036-1039.
[2006]高长生,郑建华,荆武兴,吴霞.基于地球引力变轨的日冕探测器轨道设计[J].宇航学报,2006(06):1152-1156.
[2006]高长生,荆武兴,张燕,黄翔宇.基于Unscented卡尔曼滤波器的近地卫星磁测自主导航[J].中国空间科学技术,2006(01):27-32.
动力学分析方面部分学术论文
[2018]陈尔康,廖欣,高长生,荆武兴.考虑刚体运动与弹体变形耦合效应的旋转导弹动力学建模[J].兵工学报,2018,39(11):2159-2171.
[2018]陈尔康,廖欣,高长生,荆武兴.旋转导弹喷气阻尼效应建模与分析[J].哈尔滨工业大学学报,2018,50(10):42-48.
[2017]廖欣,陈尔康,高长生,荆武兴.喷气阻尼效应作用下旋转导弹锥形运动分析[J].上海航天,2017,34(S1):29-35.
[2013]魏鹏鑫,荆武兴,高长生.攻防对抗机动过载关系分析[J].宇航学报,2013,34(02):179-185.
[2012]魏鹏鑫,高长生,荆武兴.基于稳定性分析的变质心再入飞行器布局参数设计[J].导弹与航天运载技术,2012(01):34-39.
[2012]高长生,姜春旺,魏鹏鑫,荆武兴.一种新型质量矩飞行器总体布局方案研究[J].飞行力学,2012,30(06):541-545.
[2011]韦文书,荆武兴,谷立祥,高长生.变质量飞行器变轨中摇摆发动机指向跟踪问题研究[J].宇航学报,2011,32(08):1746-1752.
[2009]李瑞康,荆武兴,高长生,杜华军.变质心飞行器姿态与弹道性能分析[J].宇航学报,2009,30(04):1498-1503.
[2008]高长生,荆武兴,李瑞康.提高变质心飞行器可操纵性的方法研究[J].宇航学报,2008(06):1773-1777.
[2008]高长生,荆武兴,李瑞康.质量矩再入飞行器的参数优化和性能分析[J].航空学报,2008(06):1419-1423.
[2007]李瑞康,荆武兴,高长生. 再入体变质心动力学建模与仿真分析[A]. 中国自动化学会控制理论专业委员会,2007:5.
[2018]Jianqing, Gao, Changsheng, et al. Novel Moving Mass Flight Vehicle and Its Equivalent Experiment[J]. Journal of dynamic systems, measurement, and control, 2018.
[2017]Jianqing Li,Changsheng Gao,Wuxing Jing,Yidi Fan. Nonlinear vibration analysis of a novel moving mass flight vehicle[J]. Nonlinear Dynamics,2017,90(1).
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