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浏览/检索结果: 共7条，第1-7条 帮助 限定条件 专题：大连理工大学    第一署名单位    第一作者单位    通讯作者单位     已选(0)清除 条数/页：5101520253035404550556065707580859095100   排序方式：请选择作者升序作者降序题名升序题名降序发表日期升序发表日期降序提交时间升序提交时间降序 Nonlinear receding horizon guidance for spacecraft formation reconfiguration on libration point orbits using a symplectic numerical method 期刊论文 ISA TRANSACTIONS, 2016, 卷号: 60, 页码: 38-52 作者:  Peng, Haijun;  Jiang, Xin 收藏  |  浏览/下载：4/0  |  提交时间：2019/12/09 Spacecraft formation reconfiguration  Libration point orbits  Circular restricted three body problem  Guidance strategy  Nonlinear receding horizon control  Symplectic numerical method   Adaptive surrogate model-based fast path planning for spacecraft formation reconfiguration on libration point orbits 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2016, 卷号: 54, 页码: 151-163 作者:  Peng, Haijun;  Wang, Wei 收藏  |  浏览/下载：9/0  |  提交时间：2019/12/09 Spacecraft formation reconfiguration  Fast path planning  Adaptive surrogate model  Libration point orbit  Circular restricted three-body problem   Improved Time-Varying Controller Based on Parameter Optimization for Libration-Point Orbit Maintenance 期刊论文 JOURNAL OF AEROSPACE ENGINEERING, 2016, 卷号: 29, 页码: - 作者:  Yang, Chunfeng;  Peng, Haijun;  Tan, Shujun;  Li, Yunpeng;  Chen, Biaosong 收藏  |  浏览/下载：4/0  |  提交时间：2019/12/09 Circular restricted three-body problem (CRTBP)  Libration-point orbit  Time-varying controller  Finite time  Parameter optimization  Weighting matrix   Optimal control of loose spacecraft formations near libration points with collision avoidance 期刊论文 NONLINEAR DYNAMICS, 2016, 卷号: 83, 页码: 2241-2261 作者:  Li, Mingwu;  Peng, Haijun;  Zhong, Wanxie 收藏  |  浏览/下载：4/0  |  提交时间：2019/12/09 Formation keeping  Formation reconfiguration  Libration points  Circular restricted three-body problem (CR3BP)  Collision avoidance  Penalty method  Symplectic method   Multi-objective transfer to libration-point orbits via the mixed low-thrust and invariant-manifold approach 期刊论文 NONLINEAR DYNAMICS, 2014, 卷号: 77, 页码: 321-338 作者:  Peng, Haijun;  Chen, Biaosong;  Wu, Zhigang 收藏  |  浏览/下载：2/0  |  提交时间：2019/12/09 Multi-objective optimization  Nonlinear optimal control  Symplectic algorithm  Circular restricted three-body problem  Low-thrust transfer  Invariant manifold   Optimal nonlinear feedback control of spacecraft rendezvous with finite low thrust between libration orbits 期刊论文 NONLINEAR DYNAMICS, 2014, 卷号: 76, 页码: 1611-1632 作者:  Peng, Haijun;  Jiang, Xin;  Chen, Biaosong 收藏  |  浏览/下载：1/0  |  提交时间：2019/12/09 Spacecraft rendezvous  Circular restricted three-body problem  Optimal feedback control  Finite low thrust  Libration point orbits   Surrogate-based parameter optimization and optimal control for optimal trajectory of Halo orbit rendezvous 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2013, 卷号: 26, 页码: 176-184 作者:  Peng, Haijun;  Yang, Chunfeng;  Li, Yunpeng;  Zhang, Sheng;  Chen, Biaosong 收藏  |  浏览/下载：3/0  |  提交时间：2019/12/11 Circular restricted three body problem (CRTBP)  Halo orbit rendezvous  Nonlinear optimal control  Surrogate-based optimization  Design of experiment