（1）总体设计：弹载自主侦察平台，微纳卫星等；

（2）测量与控制：多星编队飞行协同与控制，线性姿态确定，鲁棒自适应滤波；

（3）系统仿真：多系统数字交联仿真，半实物实时仿真，三维场景开发。

52批中国博士后基金项目：“敏捷卫星新型线性姿态确定方法研究”，主持已结题。

JOURNAL

（1）Deren GOND, Xiaowei SHAO,Wei LI, and Dengping DUAN. Optimal linearattitude estimators via geometricanalysis[J]. Journal of Zhejiang Univ-Sci A(Appl Phys & Eng), 2012, 12(11):873-882. (SCI)

（2）Deren GOND, Xiaowei SHAO,Wei LI, and Dengping DUAN. Optimal LinearAttitude Estimator and Its RecursiveAlgorithm var Geometric Analysis[J].Proceeding of the Institution of MechanicalEngineers, Part G, Journal ofAerospace Engineering. 2013, 227(1): 100-109.(SCI)

（3）Deren GOND, Xiaowei SHAO,Xiangliang WANG, and Dengping DUAN. SimpleMethod to Fuel-Optimal SpacecraftFormation[J]. Transaction of the JapanSociety for Aeronautical and SpaceScience. (SCI, Accepted)

（4）Wei Li, Deren Gong,Meihong Liu, Ji’an Chen, Dengping Duan. Adaptiverobust Kalman filter for relativenavigation using global position system[J].IET Radar, Sonar and Navigation,2013, 7(5): 471-479. (SCI)

（5）Xiaoliang Wang, DerenGong, Xiaowei Shao, Dengping Duan. Laser RadarRelative Navigation usingImproved Adaptive Hubber Filter[J]. ActaAstronautica, 2011, 68(11-12):1872-1880. (SCI)

（6）龚德仁, 邵晓巍, 王晓亮, 段登平. 航天器编队飞行的周期脉冲控制与燃料分析[J].上海航天, 2011, 27(5): 22-27.

（7）罗宇阳, 龚德仁*, 陈筠力, 段登平. 基于罗格里斯参数的航天器递归线性姿态估计算法[J]. 航天控制, 2012, 30(4): 37-41.

（8）周世龙，龚德仁*，段登平. CCD噪声模型在几何线性姿态估计中的应用[J].传感器与微系统, 2014. (Accepted)

CONFERENCE

（1） Xiangliang WANG, DerenGOND, and Dengping DUAN. Relative Semimajour AxisEstimation using Augmented GPSNavigation for HEO Formation[C]. 2010 5th ESAWorkshop on Satellite NavigationTechnologies and European Workshop on GNSSSignals and Signal Processing(NAVITEC), Dec. 8-10, 2010, Noordwijk, TheNetherlands. (EI)

（2）Zening Fu, Deren Gong*,Xiaowei Shao, and Dengping Duan. REOLAE: ARecursive Algorithm Based onRodrigues[C]. Preceedings of InternationalConference on Electric nformation andControl Engineering, April 15-17, 2011,Wuhan, China (EI)

（3）龚德仁, 邵晓巍, 段登平. 小卫星姿态快速机动的非奇异终端滑模控制[C]. 2011年小卫星技术交流会, 2011.11, 北京