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| 1 | Formation reconfiguration in restricted three body problem显示文摘形成在太阳地球的一条光圈轨道附近飞的重构限制了三个身体系统与推动演习被调查。为短时间重构,二推动的演习与分析、数字的方法并且开始结束被调查()方法被证明是一精力最佳二推动的所有( TI )之一重构,和精力消费独立于主要太空船的位置,并且与重构时间减少。然后,基因算法被采用优化精力消费。结果证明最佳的精力与起始、最后的轨道之间的半径差别增加,并且与重构时间减少。 | Shengping Gong Junfeng Li Hexi Baoyin Yunfeng Gao | 2007 | Acta Mechanica Sinica2007，23，3： | 7 |
| 2 | Feasibility analysis of the angular momentum reversal trajectory via hodograph method for high performance solar sails显示文摘In this paper a new phase space of hodograph method is adopted to investigate and better understand the two-dimensional angular momentum reversal(H-reversal) trajectories for high performance solar sails within a fixed cone angle.As the hodograph method and the H-reversal trajectory are not very common,both of them are briefly introduced.The relationship between them are constructed and addressed with a sample trajectory.How the phase space varies according to the sail quality and the fixed sail cone angle is also studied.Through variation of the phase space,the minimum sail lightness number can be obtained by solving a set of algebraic equations instead of a parameter optimization problem.For a given sail lightness number,there are three types of the two-dimensional possible heliocentric motion,including the spiral inward trajectories towards the Sun,the H-reversal trajectories and the directly outward escape trajectories.The boundaries that separate these different groups are easily determined by using the phase space.Finally,the method and procedures to achieve the feasible region of the H-reversal trajectory with required perihelion distance are presented in detail. | ZENG XiangYuan BAOYIN HeXi LI JunFeng GONG ShengPing | 2011 | Science China(Technological Sciences)2011，54，11： | 3 |
| 3 | Solar sailing trajectory optimization with planetary gravity assist显示文摘Significant propellant mass saving can be obtained with the use of complex multiple intermediate flyby maneuvers for conventional propulsion systems,and trip time also decreases for a portion of the proper solar sail missions.This paper discusses the performance of gravity assist(GA)in the time-optimal control problem of solar sailing with respect to sail lightness number and the energy difference between the initial and final orbit in the rendezvous problem in a two-body model,in which the GA is modeled as a substantial change in the velocity of the sailcraft at the GA time.In addition,this paper presents a method to solve the time-optimal problem of solar sailing with GA in a full ephemeris model,which introduces the third body’s gravity in a dynamic equation.This study builds a set of inner constraints that can describe the GA process accurately.Finally,this study presents an example for evaluating the accuracy and rationality of the two-body model’s simplification of GA by comparison with the full ephemeris model. | CAI XingShan LI JunFeng GONG ShengPing | 2015 | Science China(Physics,Mechanics & Astronomy)2015，58，1： | 3 |
| 4 | Review on solar sail technology显示文摘This paper reviews solar sail trajectory design and dynamics,attitude control,and structural dynamics.Within the area of orbital dynamics,methods relevant to transfer trajectory design and non-Keplerian orbit generation are discussed.Within the area of attitude control,di erent control strategies,including utilisation of solar radiation pressure and conventional actuators,are discussed.Finally,the methods of modelling structural dynamics during and after deployment are discussed,before considering possible future trends in developing of solar sailing missions. | Shengping Gong Malcolm Macdonald | 2019 | Astrodynamics2019，3，2： | 3 |
| 5 | Phosgene-Free Approaches to Catalytic Synthesis of Diphenyl Carbonate and Its Intermediates显示文摘 | Gong Jinlong Ma Xinbin Wang Shengping | 2007 | Appl Catal A2007，316，12： | 1 |
| 6 | Characterization and reactivity of stannum modified titanium silicalite TS-1 catalysts for transesterification of dimethyl oxalate with phenol显示文摘 | Ma Xinbin Gong Jinlong Wang Shengping | 2005 | J Mol Catal A:Chem2005，237，12： | 1 |
| 7 | Characterization and activity of stannum modified Hβ catalysts for transesterification of dimethyl oxalate with phenol显示文摘 | Wang Shengping Ma Xinbin Gong Jinlong | 2004 | Catal Today2004，，： | 1 |
| 8 | A comparative study of supported TiO2 catalysts and activity in ester exchange between dimethyl oxalate and phenol显示文摘 | Ma Xinbin Wang Shengping Gong Jinlong | 2004 | J Mol Catal A:Chem2004，222，12： | 1 |
| 9 | Reactivity and surface properties of silica supported molybdenum oxide catalysts for the transesterification of dimethyl oxalate with phenol显示文摘 | Ma Xinbin Gong Jinlong Wang Shengping | 2004 | Catal Commun2004，5，3： | 1 |
| 10 | Transesterification of dimethyl oxalate with phenol over MoO3/SiO2 catalysts显示文摘 | Gong Jinlong Ma Xinbin Wang Shengping | 2004 | J Mol Catal A:Chem2004，207，2： | 1 |
| 11 | A comparative study of supported TiO2catalysts and activity in ester exchange between dimethyl oxalate and phenol显示文摘 | MA Xinbin WANG Shengping GONG Jinlong | 2004 | Journal of Molecular Catalysis2004，222，： | 1 |
| 12 | Enhanced CO2 adsorption capacity and stability using CaO‐based adsorbents treated by hydration显示文摘 | Shengping Wang Hui Shen Shasha Fan Yujun Zhao Xinbin Ma Jinlong Gong | 2013 | AIChE J2013，，10： | 1 |
| 13 | Hydrogenation of dimethyl oxalate to ethylene glycol on a Cu/SiO2/cordierite monolithic catalyst: Enhanced internal mass transfer and stability显示文摘 | Hairong Yue Yujun Zhao Li Zhao Jing Lv Shengping Wang Jinlong Gong Xinbin Ma | 2011 | AIChE J2011，，9： | 1 |
| 14 | Reactivity and surface properties of silica supported molybdenum oxide catalysts for the transesterification of dimethyl oxalate with phenol显示文摘 | Xinbin Ma Jinlong Gong Shengping Wang Ning Gao Dali Wang Xia Yang Fei He | 2004 | Catalysis Communications2004，5，3： | 1 |
| 15 | Hydrogenation of dimethyl oxalate to ethylene glycol over mesoporous Cu ‐ MCM ‐41 catalysts显示文摘 | Xinbin Ma Hanwen Chi Hairong Yue Yujun Zhao Yan Xu Jing Lv Shengping Wang Jinlong Gong | 2013 | AIChE J2013，，7： | 1 |
| 16 | Fuel-optimal trajectory design using solar electric propulsion under power constraints and performance degradation显示文摘The fuel-optimal transfer trajectories using solar electric propulsion are designed considering the power constraints and solar array performance degradation.Three different performance degradation models including linear,positive and negative exponential degradations are used in the analysis of three typical rendezvous missions including Apophis,Venus and Ceres,respectively.The optimal control problem is formulated using the calculus of variations and Pontryagin’s maximum principle,which leads to a bang-bang control that is solved by indirect method combined with a homotopic technique.In demonstrating the effects of the power constraints and solar array performance degradation on the power budget and fuel consumption,the time histories of the power profile and the fuel consumptions are compared for the three missions.This study indicates that it is necessary to consider the power constraints and solar array performance degradation for the SEP-based low-thrust trajectory design,espacially for long-duration outbound flights. | ZHANG Peng LI JunFeng GONG ShengPing | 2014 | Science China(Physics,Mechanics & Astronomy)2014，57，6： | 1 |
| 17 | Cu-doped zeolites for catalytic oxidative carbonylation: The role of Br?nsted acids显示文摘 | Shouying Huang Yue Wang Zengzhu Wang Bing Yan Shengping Wang Jinlong Gong Xinbin Ma | 2012 | Applied Catalysis A General2012，，： | 1 |
| 18 | Phosgene-free approaches to catalytic synthesis of diphenyl carbonate and its intermediates显示文摘 | Gong Jinlong Ma Xinbin Wang Shengping | | 0，，： | 1 |
| 19 | Passive stability design for the solar sail on displaced orbits 显示文摘 | GONG Shengping LI Junfeng BAOYIN Hexi | 2007 | Journal of Spacecraft and Rockets2007，44，5： | 1 |
| 20 | Analysis of displaced solar sail orbits 显示文摘 | GONG Shengping LI Junfeng BAOYIN Hexi | 2008 | Journal of Guidance Control and Dynamics2008，31，3： | 1 |
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