Design and simulation of transfer orbit for space exploration using lagrange points

机译：使用拉格朗日点传输轨道传输轨道的设计与仿真

获取原文

页面导航

摘要
著录项
相似文献
相关主题

摘要

For the space exploration program, it is very important to launch a satellite into a satisfactory halo orbit with the required minimum cost. This paper presents three kinds of Poincare? sections based on the invariant manifold theory, and chooses the optimal one to design the transfer orbit of Halo orbit from earth to L1 point, and analyzes the effect of parameters. The simulation results show that the lower cost transfer orbit can be designed by choosing proper Poincare? sections.

机译：对于空间探索计划，将卫星发射成令人满意的光环轨道是非常重要的，所需的最低成本是非常重要的。本文呈现了三种庞的诗句？基于不变的歧管理论的部分，并选择从地球到L1点设计光环轨道的转移轨道的最佳轨道，并分析参数的效果。仿真结果表明，较低的成本转移轨道可以通过选择适当的POINCARE来设计？部分。

著录项

来源
《IEEE Chinese Guidance, Navigation and Control Conference》|2016年|1 v.|共5页
会议地点
作者
Li Ze; Li Yonghua; Wang Xiaoting;
展开▼
作者单位

展开▼
会议组织
原文格式 PDF
正文语种
中图分类飞行控制系统与导航;
关键词
Orbits; Manifolds; Earth; Space vehicles; Vibrations; Space exploration; Satellites;

机译：轨道;歧管;地球;太空车辆;振动;太空探索;卫星;

相似文献

外文文献
中文文献
专利

1. Deep space exploration orbit design departing from circumlunar orbit of lunar base [J] . Qiu Shi, Cao Xibin, Wang Feng, Aerospace science and technology . 2019,第Deca期

机译：脱离月球周圆轨道的深空探测轨道设计
2. Cloud-Based CAD Parametrization for Design Space Exploration and Design Optimization in Numerical Simulations [J] . Joel Guerrero, Luca Mantelli, Sahrish B. Naqvi Fluids . 2020,第1期

机译：基于云的CAD参数化设计空间探索和设计优化在数值模拟中
3. Proficient Design Space Exploration of ZYNQ SoC using VIVADO Design Suite: Custom Design of High Performance AXI Interface for High speed data transfer between PL and DDR Memory using Hardware-Software Co-Design [J] . Rikin J. Nayak, Jaiminkumar B. Chavda International Journal of Applied Engineering Research . 2018,第11aPta2期

机译：使用Vivado设计套件熟练设计空间探索Zynq SoC：高性能AXI接口的定制设计，用于使用硬件 - 软件共同设计的PL和DDR内存高速数据传输
4. Design and simulation of transfer orbit for space exploration using lagrange points [C] . Li Ze, Li Yonghua, Wang Xiaoting IEEE Chinese Guidance, Navigation and Control Conference . 2016

机译：利用拉格朗日点进行空间探索的转移轨道的设计与仿真
5. Spacecraft transfer trajectory design exploiting resonant orbits in multi-body environments. [D] . Vaquero Escribano, Tatiana Mar. 2013

机译：利用多体环境中的共振轨道的航天器转移轨迹设计。
6. Industrial application of heat- and mass balance model for fluid-bed granulation for technology transfer and design space exploration [O] . David R. Ochsenbein, Matthew Billups, Bingbing Hong, 2019

机译：流化床制粒热质平衡模型在工业中的技术应用及设计空间探索
7. Cloud-Based CAD Parametrization for Design Space Exploration and Design Optimization in Numerical Simulations [O] . Joel Guerrero, Luca Mantelli, Sahrish B. Naqvi 2020

机译：基于云的CAD参数化设计空间探索和设计优化在数值模拟中
8. Military Space Mission Design and Analysis in a Multi-Body Environment: An Investigation of High-Altitude Orbits as Alternative Transfer Paths, Parking Orbits for Reconstitution, and Unconventional Mission Orbits. [R] . Brick, J. N. 2017

机译：多体环境中的军事太空任务设计与分析：高空轨道作为替代传递路径，重建停车轨道和非常规任务轨道的调查。

Design and simulation of transfer orbit for space exploration using lagrange points

摘要

著录项

相似文献

相关主题

期刊订阅