| A sequential surrogate method for reliability analysis based on radial basis function X Li, C Gong, L Gu, W Gao, Z Jing, H Su Structural Safety 73, 42-53, 2018 | 106 | 2018 |
| A cooperative radial basis function method for variable-fidelity surrogate modeling X Li, W Gao, L Gu, C Gong, Z Jing, H Su Structural and Multidisciplinary Optimization 56, 1077-1092, 2017 | 30 | 2017 |
| Hp-adaptive RPD based sequential convex programming for reentry trajectory optimization T Zhang, H Su, C Gong Aerospace Science and Technology 130, 107887, 2022 | 25 | 2022 |
| An efficient space division–based width optimization method for RBF network using fuzzy clustering algorithms Y Zhang, C Gong, H Fang, H Su, C Li, A Da Ronch Structural and Multidisciplinary Optimization 60, 461-480, 2019 | 22 | 2019 |
| A surrogate model based nested optimization framework for inverse problem considering interval uncertainty H Fang, C Gong, C Li, X Li, H Su, L Gu Structural and Multidisciplinary Optimization 58, 869-883, 2018 | 20 | 2018 |
| Research on geometry modeling method based on three-dimensional CST parameterization technology H Su, L Gu, C Gong 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 3241, 2015 | 19 | 2015 |
| A gradient-based uncertainty optimization framework utilizing dimensional adaptive polynomial chaos expansion H Fang, C Gong, H Su, Y Zhang, C Li, A Da Ronch Structural and Multidisciplinary Optimization 59, 1199-1219, 2019 | 12 | 2019 |
| Finite Time Distributed Synchronization of Spacecraft Formation Attitude with Complex Constraints J Zhou Journal of Astronautics 39 (12), 1340, 2018 | 8* | 2018 |
| Three‐Dimensional CST Parameterization Method Applied in Aircraft Aeroelastic Analysis H Su, C Gong, L Gu International Journal of Aerospace Engineering 2017 (1), 1874729, 2017 | 8 | 2017 |
| A three-stage sequential convex programming approach for trajectory optimization T Zhang, H Su, C Gong Aerospace Science and Technology 149, 109128, 2024 | 7 | 2024 |
| 非匹配不确定性条件下的编队分布式协同控制. 周健， 龚春林， 谷良贤， 粟华 Systems Engineering & Electronics 41 (3), 2019 | 7 | 2019 |
| Review of UMDO for system design of flight vehicle M ZHAO Journal of astronautics 39 (6), 593, 2018 | 7* | 2018 |
| 亚轨道重复使用运载器总体多学科优化方法 龚春林， 谷良贤， 粟华 固体火箭技术 35 (1), 5-10, 2012 | 7 | 2012 |
| A novel linear uncertainty propagation method for nonlinear dynamics with interval process L Zhang, C Li, H Su, X Wang, C Gong Nonlinear Dynamics 111 (5), 4425-4450, 2023 | 6 | 2023 |
| Multidisciplinary design optimization method for suborbital reusable launch vehicle CL Gong, LX Gu, H Su Journal of Solid Rocket Technology(JSRT) 35 (1), 5-10, 2012 | 6 | 2012 |
| Hybrid simulated annealing algorithm based on the parallel strategy S Hua, G Liangxian, G Chunlin 2010 International Symposium on Computational Intelligence and Design 2, 102-105, 2010 | 5 | 2010 |
| 本征正交分解在翼型气动优化中的应用研究 李波， 龚春林， 粟华， 谷良贤 上海航天 34 (5), 117-123, 2017 | 4 | 2017 |
| 基于 CAD 的半解析参数化几何建模方法 黎旭， 龚春林， 谷良贤， 粟华 计算机与现代化, 1, 2014 | 4 | 2014 |
| 基于三维 CST 建模方法的两层气动外形优化策略 粟华， 龚春林， 谷良贤 固体火箭技术 37 (1), 1-6, 2014 | 4 | 2014 |
| Static aeroelastic optimization of hypersonic aircraft based on high-fidelity model SU Hua, GU Liang-xian, G Chun-lin 航空动力学报 28 (8), 1836-1842, 2013 | 4 | 2013 |
