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北京航空航天大学 [9]
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Maintenance of Libration Point Orbit in Elliptic Sun-Mercury Model
期刊论文
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2018, 卷号: 54, 页码: 144-158
作者:
Peng, Hao
;
Liao, Yuxin
;
Bai, Xiaoli
;
Xu, Shijie
收藏
  |  
浏览/下载:10/0
  |  
提交时间:2019/12/30
Intelligent systems
Maintainability
Maintenance
Mathematical models
Mercury (metal)
Monte Carlo methods
Orbits
Sun
Trajectories
Libration point orbits
Mercury system
Orbit maintenance
Receding horizon control
Restricted three body problem
Space vehicles
Interplanetary flight
Natural formation flying on quasi-halo orbits in the photogravitational circular restricted three-body problem
期刊论文
ACTA ASTRONAUTICA, 2018, 卷号: 149, 页码: 35-46
作者:
Luo, Tong
;
Xu, Ming
;
Dong, Yunfeng
收藏
  |  
浏览/下载:3/0
  |  
提交时间:2019/12/30
Formation flying
Quasi-halo orbits
Three-body problem
Libration point
Center manifold
Poincare mapping
Study of Time-Free Transfers into Libration Point Orbits with Multiple Constraints
期刊论文
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2017, 卷号: 40, 期号: 11, 页码: 2752-2770
作者:
Zeng, Hao
;
Zhang, Jingrui
;
Qi, Rui
;
Li, Mingtao
;
Zeng, H (reprint author), Beijing Inst Technol, Sch Aerosp Engn, 5 Zhongguancun South Str, Beijing 100081, Peoples R China.
收藏
  |  
浏览/下载:19/0
  |  
提交时间:2017/12/19
A fast multi-objective optimization design method for emergency libration point orbits transfer between the Sun-Earth and the Earth-Moon systems
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 63, 页码: 152-166
作者:
Wang, Wei
;
Peng, Haijun
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  |  
浏览/下载:5/0
  |  
提交时间:2019/12/02
Libration point
Transfer trajectory design
Multi-objective optimization
Adaptive surrogate model
Sun-Earth system
Earth-Moon system
Multiple Spacecraft Formation Flying Control around Sun-Earth L-2 Libration Point
期刊论文
2017 32ND YOUTH ACADEMIC ANNUAL CONFERENCE OF CHINESE ASSOCIATION OF AUTOMATION (YAC), 2017, 页码: 120-126
作者:
Lou, Zhangpeng
;
Li, Teng
;
Yin, Yating
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  |  
浏览/下载:5/0
  |  
提交时间:2019/04/24
Spacecraft Formation Flying
Libration Point Orbits
Active Disturbance Rejection Control
Lunar flyby transfers between libration point orbits
期刊论文
MONTHLY NOTICES OF THE ROYAL ASTRONOMICAL SOCIETY, 2017, 卷号: 468, 页码: 2265-2282
作者:
Qi, Yi
;
Xu, Shijie
;
Qi, Rui
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  |  
浏览/下载:2/0
  |  
提交时间:2019/12/30
methods: numerical
space vehicles
Moon
celestial mechanics
planets and satellites: general
Formation flying on quasi-halo orbits in restricted Sun-Earth/Moon system
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 67, 页码: 118-125
作者:
Xu, Ming
;
Liang, Yuying
;
Fu, Xiaoyu
收藏
  |  
浏览/下载:11/0
  |  
提交时间:2019/12/30
Hamiltonian structure-preserving control
Formation flying
Bi-circular model
Quasi-halo orbits
Libration point
IMPULSIVE HALO TRANSFER TRAJECTORY DESIGN AROUND SEL1 POINT WITH MULTIPLE CONSTRAINTS
会议论文
AAS/AIAA Astrodynamics Specialist Conference, Vail, CO, AUG 11-13, 2015
作者:
Zeng, Hao
;
Zhang, Jingrui
;
Li, Mingtao
;
Guo, Zixi
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  |  
浏览/下载:23/0
  |  
提交时间:2016/12/29
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
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