全部 标题 作者
关键词 摘要

OALib Journal期刊
ISSN: 2333-9721
费用:99美元

查看量下载量

相关文章

更多...
力学学报  2015 

基于虚拟中心引力场方法的航天器转移轨道设计

DOI: 10.6052/0459-1879-14-112, PP. 180-184

Keywords: 轨道机动,转移轨道,连续推力,中心引力场

Full-Text   Cite this paper   Add to My Lib

Abstract:

空间机动技术是实现空间操作任务的基础,具有重要的研究价值.研究了连续推力作用下航天器转移轨道设计问题,提出了一种基于虚拟中心引力场的轨道设计方法.该方法有两大特点(1)能够将机动轨道设计问题转化为虚拟中心引力场参数的优化问题,简化了设计过程;(2)对轨道形状或推力方向、大小不做任何假定,能够应用于一般情况下的机动轨道设计.将该方法应用于航天器二维和三维的转移轨道设计,并和形状方法进行了对比分析.仿真结果分析表明,采用该方法简化了轨道设计过程,为航天器快速轨道设计提供了新思路.

References

[1]  李俊峰,蒋方华,连续小推力航天器的深空探测轨道优化方法综述,力学与实践,2011, 33(3): 1-6 (Li Junfeng, Jiang Fanghua. Survey of low-thrust trajectory optimization methods for deep space exploration. Mechanics and Engineering, 2011, 33(3): 1-6 (in Chinese))
[2]  汤国建,张洪波. 小推力轨道机动动力学与控制,北京:科学出版社,2013 (Tang Guojian, Zhang Hongbo. Dynamics and Control of Low-thrust Orbital Maneuver. Beijing: Science Press,2013 (in Chinese))
[3]  Tisen H. Take-off from satellite orbit. Journal of the American Rocket Society, 1953, 23(4): 233-236
[4]  Boltz FW. Orbit motion under continuous radial thrust. Journal of Guidance, Control, and Dynamics, 1991, 14(3): 667-670;
[5]  Petropoulos AE, Longuski JM. Automated design of low-thrust gravity-assist trajectories. Journal of Spacecraft and Rockets, 2004, 41(5): 787-796
[6]  Bradley W. Shape-based approximation method for low-thrust trajectory optimization. AIAA 2008-6616, 2008. 1-9
[7]  Wall BJ, Conway BA. Shape-based approach to low-thrust rendezvous trajectory design. Journal of Guidance, Control, and Dynamics, 2009, 32 (1): 95-101
[8]  Hudson J, Scheeres D. Fourier coefficient selection for low-thrust control shaping. Journal of Guidance, Control, and Dynamics, 2013, 36 (6): 1783-1786
[9]  潘峰,李位星. 粒子群优化算法与多目标优化. 北京:北京理工大学出版社,2013(Pan Feng, Li Weixing. Particle Swarm Optimization Algorithm and Multiply Variables Optimization. Beijing: Beijing Institute of Technology Press, 2013 (in Chinese))

Full-Text

Contact Us

service@oalib.com

QQ:3279437679

WhatsApp +8615387084133