位置：成果数据库 > 期刊 > 期刊详情页
Feasibility analysis of the angular momentum reversal trajectory via hodograph method for high perfo
  • ISSN号：1674-7321
  • 期刊名称：Science in China - Series E: Technological Science
  • 时间：0
  • 页码：2951-2957
  • 相关项目：深空探测中若干非线性动力学与控制问题
作者： Zeng XiangYuan|Baoyin HeXi|Li JunFeng|Gong ShengPing|
同期刊论文项目
深空探测中若干非线性动力学与控制问题
期刊论文 85 获奖 2
同项目期刊论文
Satellite scheduling considering maximum observation coverage time and minimum orbital transfer fuel
Two-Point Boundary Value Problem Solutions to Spacecraft Formation Flying
Multi-Satellite Reconfiguration of Formation around Libration Point
Capturing near earth objects
基于形状的行星际小推力转移轨道初始设计方法
Five Special Types of Orbits Around Mars
星际探测多脉冲转移发射机会搜索方法研究
Practical Techniques for Low-Thrust Trajectory Optimization with Homotopic Approach
New applications of the H-reversal trajectory using solar sails
Utilization of an H-reversal trajectory of a solar sail for asteroid deflection
Dynamic modelling and analysis of space webs
结合行星借力飞行技术的小推力转移轨道初始设计
小推力下卫星编队的非自然构型设计与控制
Solar sail transfer trajectory from L1 point to sub-L1 point
Solar sail time-optimal interplanetary transfer trajectory design
精确动力学模型下的火星探测轨道设计
小行星探测目标选择与转移轨道方案设计
Collision criterion for two satellites on Keplerian orbits
Target selection and transfer trajectories design for exploring asteroid mission
基于椭圆型限制性三体模型的借力飞行机理研究
2005～2009年国际深空轨迹优化竞赛综述
基于高斯伪光谱的星际小推力转移轨道快速优化
星际探测借力飞行轨道的混合设计方法研究
Reachable Domain for Spacecraft with a Single Impulse
Control of large angle maneuvers for the flexible solar sail
The elastic contact influences on passive walking gaits
Reduced Model for Flexible Solar Sail Dynamics
连续小推力航天器的深空探测轨道优化方法综述
小天体伴飞的常推力控制
Coupled trajectory and attitude stability of displaced orbits
Formation flying solar-sail gravity tractors in displaced orbit for towing near-Earth asteroids
The design of transfer trajectory for Ivar asteroid exploration mission
考虑太阳引力摄动的Halo轨道保持控制
Solar radiation pressure used for formation flying control around the Sun-Earth libration point
非开普勒轨道动力学与控制
Transfer Trajectories Design for a Variable Lightness Solarcraft
Coupled attitude-orbit dynamics and control for displaced solar orbits
Homotopic approach and pseudospectral method applied jointly to low thrust trajectory optimization
基于B平面的火星探测直接转移轨道设计方法
横向连续推力小偏心率人工冻结轨道设计
含滚阻摩擦平面多体系统的建模和数值方法
第三届全国深空轨道设计竞赛总结
深空探测自主导航技术综述
嫦娥二号日地拉格朗日L2点探测轨道设计与实施
Analytic approach on geometric structure of invariant manifolds of the collinear Lagrange points
太阳帆绕地球周期轨道研究
A curved surface solar radiation pressure force model for solar sail deformation
Receding Horizon-Based Dual Control Strategy for Pinpoint Planetary Landing
Sensitivity analysis for a type of statically stable sailcrafts
Periodic orbits based on geometric structure of center manifold around Lagrange points
非光滑多体系统动力学数值算法的研究进展
Multi-swingby optimization of mission to Saturn using global optimization algorithms
从月球逃逸探测小行星的发射机会搜索
光压摄动对卫星姿态轨道耦合的影响分析
木星探测轨道分析与设计
利用太阳光压力进行Halo轨道编队控制
三维引力辅助解析分析方法研究
Trajectory optimization and applications using high performance solar sails
柔性太阳帆航天器大角度机动控制研究