Space Very Long Baseline Interferometry(S-VLBI) is an aperture synthesis technique utilizing an array of radio telescopes including ground telescopes and space orbiting telescopes.It can achieve much higher spatial re...Space Very Long Baseline Interferometry(S-VLBI) is an aperture synthesis technique utilizing an array of radio telescopes including ground telescopes and space orbiting telescopes.It can achieve much higher spatial resolution than that from the ground-only VLBI.In this paper,a new concept of twin spacecraft S-VLBI has been proposed,which utilizes the space-space baselines formed by two satellites to obtain larger and uniform uv coverage without atmospheric influence and hence achieve high quality images with higher angular resolution.The orbit selections of the two satellites are investigated.The imaging performance and actual launch conditions are all taken into account in orbit designing of the twin spacecraft S-VLBI.Three schemes of orbit design using traditional elliptical orbits and circular orbits are presented.These design results can be used for different scientific goals.Furthermore,these designing ideas can provide useful references for the future Chinese millimeter-wave S-VLBI mission.展开更多
On-orbit service spacecraft orbit problem has been addressed for decades. The research of on-orbit service spacecraft orbit can be roughly divided into orbit design and orbit optimization. The paper mainly focuses on ...On-orbit service spacecraft orbit problem has been addressed for decades. The research of on-orbit service spacecraft orbit can be roughly divided into orbit design and orbit optimization. The paper mainly focuses on the orbit design problem. We simply summarize of the previous works, and point out the main content of the on-orbit service spacecraft orbit design. We classify current on-orbit service spacecraft orbit design problem into parking-orbit design, maneuvering-orbit design and servicing-orbit design. Then, we give a detail description of the three specific orbits, and put forward our own ideas on the existed achievements. The paper will provide a meaningful reference for the on-orbit service spacecraft orbital design research.展开更多
The asteroid exploration opportunities are searched and calculated with launch dates in 2006 to2010, and with asteroid Ivar 1627 as the target, the spacecraft and its subsystems are designed and analyzed,and the trans...The asteroid exploration opportunities are searched and calculated with launch dates in 2006 to2010, and with asteroid Ivar 1627 as the target, the spacecraft and its subsystems are designed and analyzed,and the transfer trajectory is designed using △VEGA technology for the asteroid rendezvous. The design resultssatisfied the energy requirements for small explorers.展开更多
With the sharp increase of China＇s in-orbit spacecraft and the constraint TT＆C resources, a mathematical model for optimal TT＆C resource allocation is proposed, and the TT＆C facility remote monitoring function is ...With the sharp increase of China＇s in-orbit spacecraft and the constraint TT＆C resources, a mathematical model for optimal TT＆C resource allocation is proposed, and the TT＆C facility remote monitoring function is designed to achieve the multitask operation pattern under the unified management of the network management center. With this pattern, the TT＆C network management and the spacecraft management are separated, which is quite different from the previous pattern. Further, a novel spacecraft TT＆C technique based on spacecraft control language is developed, and the telecommanding pattern is designed to address the spacecraft operation problems. The engineering application shows that this pattern fundamentally improves the TT＆C network capability, increases the resource efficiency, and satisfies the efficient, accurate, and flexible operation of spacecraft.展开更多
为了适应未来大型复杂系统设计与功能分析需求,在火星维护与管理装置设计中引入了基于模型的系统工程(model-based system engineering,MBSE)方法。首先,基于MagicDraw系统建模工具,利用SysML建模语言,以火星表面维护与管理装置为例,从...为了适应未来大型复杂系统设计与功能分析需求,在火星维护与管理装置设计中引入了基于模型的系统工程(model-based system engineering,MBSE)方法。首先,基于MagicDraw系统建模工具,利用SysML建模语言,以火星表面维护与管理装置为例,从概念层、逻辑层和物理层逐层分解,对火星维护与管理装置进行总体设计,提出火星车和智能机器人两种物理实现方案。随后,为对设计方案进行追溯性验证,建立了从用户需求到系统逻辑架构和指标能力的需求精化映射矩阵。结果表明,火星维护与管理装置的MBSE功能架构设计方法充分保证了用户需求和装置功能架构的紧密结合,提高了系统设计的可追溯性,可为MBSE方法在航天器总体设计提供应用参考。展开更多
基金Supported by the Natural Science Foundation of China(40701100,40801136)the Strategic Priority Program on Space Science of the Chinese Academy of Sciences(XDA04060803)
文摘Space Very Long Baseline Interferometry(S-VLBI) is an aperture synthesis technique utilizing an array of radio telescopes including ground telescopes and space orbiting telescopes.It can achieve much higher spatial resolution than that from the ground-only VLBI.In this paper,a new concept of twin spacecraft S-VLBI has been proposed,which utilizes the space-space baselines formed by two satellites to obtain larger and uniform uv coverage without atmospheric influence and hence achieve high quality images with higher angular resolution.The orbit selections of the two satellites are investigated.The imaging performance and actual launch conditions are all taken into account in orbit designing of the twin spacecraft S-VLBI.Three schemes of orbit design using traditional elliptical orbits and circular orbits are presented.These design results can be used for different scientific goals.Furthermore,these designing ideas can provide useful references for the future Chinese millimeter-wave S-VLBI mission.
基金Supported by National Natural Science Foundation of China(Nos.60875046,61202251)Program for Changjiang Scholars and Innovative Research Team in University(No.IRT1109)+4 种基金Key Project of Chinese Ministry of Education(No.209029)Program for Liaoning Excellent Talents in University(No.LR201003)Program for Liaoning Science and Technology Research in University(Nos.LS2010008,LS2010179)Program for Liaoning Innovative Research Team in University(No.LT2011018)Doctoral Fund of Dalian University
文摘On-orbit service spacecraft orbit problem has been addressed for decades. The research of on-orbit service spacecraft orbit can be roughly divided into orbit design and orbit optimization. The paper mainly focuses on the orbit design problem. We simply summarize of the previous works, and point out the main content of the on-orbit service spacecraft orbit design. We classify current on-orbit service spacecraft orbit design problem into parking-orbit design, maneuvering-orbit design and servicing-orbit design. Then, we give a detail description of the three specific orbits, and put forward our own ideas on the existed achievements. The paper will provide a meaningful reference for the on-orbit service spacecraft orbital design research.
文摘The asteroid exploration opportunities are searched and calculated with launch dates in 2006 to2010, and with asteroid Ivar 1627 as the target, the spacecraft and its subsystems are designed and analyzed,and the transfer trajectory is designed using △VEGA technology for the asteroid rendezvous. The design resultssatisfied the energy requirements for small explorers.
基金supported by the China Postdotoral Science Foundation (20060401004).
文摘With the sharp increase of China＇s in-orbit spacecraft and the constraint TT＆C resources, a mathematical model for optimal TT＆C resource allocation is proposed, and the TT＆C facility remote monitoring function is designed to achieve the multitask operation pattern under the unified management of the network management center. With this pattern, the TT＆C network management and the spacecraft management are separated, which is quite different from the previous pattern. Further, a novel spacecraft TT＆C technique based on spacecraft control language is developed, and the telecommanding pattern is designed to address the spacecraft operation problems. The engineering application shows that this pattern fundamentally improves the TT＆C network capability, increases the resource efficiency, and satisfies the efficient, accurate, and flexible operation of spacecraft.
文摘为了适应未来大型复杂系统设计与功能分析需求,在火星维护与管理装置设计中引入了基于模型的系统工程(model-based system engineering,MBSE)方法。首先,基于MagicDraw系统建模工具,利用SysML建模语言,以火星表面维护与管理装置为例,从概念层、逻辑层和物理层逐层分解,对火星维护与管理装置进行总体设计,提出火星车和智能机器人两种物理实现方案。随后,为对设计方案进行追溯性验证,建立了从用户需求到系统逻辑架构和指标能力的需求精化映射矩阵。结果表明,火星维护与管理装置的MBSE功能架构设计方法充分保证了用户需求和装置功能架构的紧密结合,提高了系统设计的可追溯性,可为MBSE方法在航天器总体设计提供应用参考。
