混合小推力航天器日心悬浮轨道保持控制

doi:10.7527/S1000-6893.2015.0138

电子与控制

本期目录 | 过刊浏览 | 高级检索

前一篇 | 后一篇

混合小推力航天器日心悬浮轨道保持控制

张楷田, 楼张鹏, 王永, 陈绍青

中国科学技术大学自动化系, 合肥 230027

收稿日期:2015-01-06 修回日期:2015-05-25 出版日期:2015-12-15 发布日期:2015-06-01
通讯作者: 王永,Tel.:0551-63601506,E-mail:yongwang@ustc.edu.cn E-mail:yongwang@ustc.edu.cn
作者简介:张楷田,男,硕士研究生。主要研究方向:太阳帆航天器轨道动力学与控制,E-mail:zktaf@mail.ustc.edu.cn;楼张鹏,男,博士研究生。主要研究方向:太阳帆航天器轨道动力学与控制,E-mail:louzp@mail.ustc.edu.cn;王永,男,博士,教授,博士生导师。主要研究方向:运动体控制,振动主动控制,飞行器制导与控制,机器人控制,信息融合。Tel:0551-63601506,E-mail:yongwang@ustc.edu.cn;陈绍青,男,博士,工程师。主要研究方向:振动主动控制,自适应控制,E-mail:windcsq@ustc.edu.cn

Station-keeping control of spacecraft using hybrid low-thrust propulsion in heliocentric displaced orbits

ZHANG Kaitian, LOU Zhangpeng, WANG Yong, CHEN Shaoqing

Department of Automation, University of Science and Technology of China, Hefei 230027, China

Received:2015-01-06 Revised:2015-05-25 Online:2015-12-15 Published:2015-06-01

摘要/Abstract

摘要：

针对太阳帆、太阳电混合推进航天器日心悬浮轨道保持控制问题进行了研究。为解决基于局部线性化模型设计轨道保持控制器时存在的控制精度不高、模型精确性过度依赖等问题,应用自抗扰控制(ADRC)技术设计了轨道保持控制器。首先,采用圆形限制性三体问题(CRTBP)模型推导了混合小推力航天器日心悬浮轨道动力学方程;然后,考虑系统模型不确定性和外部扰动,提出了一种基于扰动估计和补偿的轨道保持控制方法;最后,数值仿真表明存在系统模型不确定性、初始入轨误差及地球轨道偏心率扰动等因素的情况下,所设计的控制器仅需很小的速度增量即可实现高精度的日心悬浮轨道保持控制。

关键词: 混合小推力, 太阳帆, 日心悬浮轨道, 轨道保持, 自抗扰控制

Abstract:

In this paper, station-keeping of heliocentric displaced orbits using a hybrid of solar sail and solar electric propulsion is investigated. In order to avoid the problem of low control precision and excessive dependence on model accuracy, which occurs when controllers are designed according to locally linearized models, a station-keeping control method based on active disturbance rejection control (ADRC) technique is proposed. Firstly, the dynamic model of a spacecraft using hybrid low-thrust propulsion in the heliocentric displaced orbit is derived based on the circular restricted three-body problem (CRTBP). Secondly, considering unmodelled dynamic and external disturbance, a station-keeping control method based on disturbance estimation and compensation is then presented. Finally, numerical simulations show that in the presence of system uncertainties, initial injection errors, and perturbations of the eccentric nature of the Earth's orbit, high station-keeping control precision can be achieved with relative small velocity increment.

Key words: hybrid low-thrust propulsion, solar sails, heliocentric displaced orbit, station-keeping, active disturbance rejection control

中图分类号:

V448.2

张楷田, 楼张鹏, 王永, 陈绍青. 混合小推力航天器日心悬浮轨道保持控制[J]. 航空学报, 2015, 36(12): 3910-3918.

ZHANG Kaitian, LOU Zhangpeng, WANG Yong, CHEN Shaoqing. Station-keeping control of spacecraft using hybrid low-thrust propulsion in heliocentric displaced orbits[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(12): 3910-3918.

参考文献

[1] McInnes C R, McDonald A, Simmons J, et al. Solar sail parking in restricted three-body system[J]. Journal of Guidance, Control, and Dynamics, 1994, 17(2):399-406.
[2] Baoyin H X, McInnes C R. Solar sail equilibria in the elliptical restricted three-body problem[J]. Journal of Guidance, Control, and Dynamics, 2006, 29(3):538-543.
[3] Baoyin H X, McInnes C R. Solar sail halo orbits at the sun-earth artificial L1 point[J]. Celestial Mechanics and Dynamical Astronomy, 2006, 94(2):155-171.
[4] Gong S P, Li J F, Baoyin H X. Analysis of displaced solar sail orbits with passive control[J]. Journal of Guidance, Control, and Dynamics, 2008, 31(3):782-785.
[5] Heiligers J, McInnes C R, Biggs J D, et al. Displaced geostationary orbits using hybrid low-thrust propulsion[J]. Acta Astronautica, 2012, 71:51-67.
[6] Simo J, McInnes C R. Designing displaced lunar orbits using low-thrust propulsion[J]. Journal of Guidance, Control, and Dynamics, 2010, 33(1):259-265.
[7] McKay R, Macdonald M, Biggs J, et al. Survey of highly non-Keplerian orbits with low-thrust propulsion[J]. Journal of Guidance, Control, and Dynamics, 2011, 34(3):645-666.
[8] McInnes C R. Passive control of displaced solar sail orbits[J]. Journal of Guidance, Control, and Dynamics, 1998, 21(6):975-982.
[9] Bookless J, McInnes C. Dynamics and control of displaced periodic orbits using solar-sail propulsion[J]. Journal of Guidance, Control, and Dynamics, 2006, 29(3):527-537.
[10] Simo J, McInnes C R. Feedback stabilization of displaced periodic orbits:Application to binary asteroids[J]. Acta Astronautica, 2014, 96:106-115.
[11] Gong S P, Baoyin H X, Li J F. Solar sail formation flying around displaced solar orbits[J]. Journal of Guidance, Control, and Dynamics, 2007, 30(4):1148-1152.
[12] Qian H, Zheng J H, Yu X Z, et al. Dynamics and control of displaced orbits for solar sail spacecraft[J]. Chinese Journal of Space Science, 2013, 33(4):458-464(in Chinese).钱航,郑建华,于锡峥,等.太阳帆航天器悬浮轨道动力学与控制[J].空间科学学报, 2013, 33(4):458-464.
[13] Zhang H, Zhu M, Zhou J L, et al. Station-keeping control of solar sail Lissajous orbit with attitude angles amplitude constraint[J]. Chinese Journal of Space Science, 2014, 34(6):872-880(in Chinese).张辉,朱敏,周建亮,等.姿态角幅值约束下的太阳帆Lissajous轨道保持控制[J].空间科学学报, 2014, 34(6):872-880.
[14] Zhang J, Wang T S. Coupled attitude-orbit control of flexible solar sail for displaced solar orbit[J]. Journal of Spacecraft and Rockets, 2013, 50(3):675-685.
[15] Luo C, Zheng J H, Gao D. Study on orbit dynamics and control of solar-sail spacecraft[J]. Journal of Astronautics, 2009, 30(6):2111-2117(in Chinese).罗超,郑建华,高东.太阳帆航天器的轨道动力学和轨道控制研究[J].宇航学报, 2009, 30(6):2111-2117.
[16] Gong S P. Study on dynamics and control of sail-craft[D]. Beijing:Tsinghua University, 2009(in Chinese).龚胜平.太阳帆航天器动力学与控制研究[D].北京:清华大学, 2009.
[17] Liu L, Hou X Y. Dynamics in deep space exploration[M]. Beijing:Publishing House of Electronic Industry, 2012:50-51(in Chinese).刘林,候锡云.深空探测器轨道力学[M].北京:电子工业出版社, 2012:50-51.
[18] Han J Q. Active disturbance rejection controller and its applications[J]. Control and Decision, 1998, 13(1):19-23(in Chinese).韩京清.自抗扰控制及其应用[J].控制与决策, 1998, 13(1):19-23.
[19] Kulkarni J E, Campbell M E, Dullerud G E. Stabilization of spacecraft flight in halo orbits:An H_∞ approach[J]. IEEE Transactions on Control Systems Technology, 2006, 14(3):572-578.
[20] McKay R J, Macdonald M, Bosquillon de Frescheville F, et al. Non-keplerian orbits using low thrust, high ISP propulsion systems[C]//Proceedings of the 60th International Astronautical Congress. Paris:IAF, 2009.
[21] Peng H, Zhao J, Wu Z, et al. Optimal periodic controller for formation flying on libration point orbits[J]. Acta Astronautica, 2011, 69(7):537-550.

E-mail：hkxb@buaa.edu.cn

关于我们

期刊社服务

专业学科

封面文章

友情链接

主管单位：中国科学技术协会主办单位：中国航空学会北京航空航天大学

混合小推力航天器日心悬浮轨道保持控制

Station-keeping control of spacecraft using hybrid low-thrust propulsion in heliocentric displaced orbits

PDF (PC)

可视化

摘要/Abstract

引用本文

使用本文

参考文献

相关文章 15

编辑推荐

Metrics

本文评价

[1]	李霞, 齐国元, 郭曦彤, 赵旭. 高阶微分反馈控制及在四旋翼飞行器中的应用[J]. 航空学报, 2022, 43(12): 326047-326047.
[2]	吴正平, 邓聪, 文海. 模糊线性/非线性自抗扰切换控制及其应用[J]. 航空学报, 2021, 42(9): 324710-324710.
[3]	武云丽, 赵天一, 左华平, 孟斌. 地球同步轨道薄膜太阳帆的姿态轨道控制方法[J]. 航空学报, 2020, 41(S2): 724291-724291.
[4]	朴敏楠, 陈志刚, 孙明玮, 陈增强. 高超声速飞行器气动伺服弹性的自适应抑制[J]. 航空学报, 2020, 41(11): 623698-623698.
[5]	费伦, 段海滨, 徐小斌, 鲍瑞, 孙永斌. 基于变权重变异鸽群优化的无人机空中加油自抗扰控制器设计[J]. 航空学报, 2020, 41(1): 323490-323490.
[6]	陈弈澄, 齐瑞云, 张嘉芮, 王焕杰. 混合小推力航天器轨道保持高性能滑模控制[J]. 航空学报, 2019, 40(7): 322827-322827.
[7]	韦常柱, 琚啸哲, 徐大富, 吴荣, 崔乃刚. 垂直起降重复使用运载器返回制导与控制[J]. 航空学报, 2019, 40(7): 322782-322782.
[8]	吴文海, 高阳, 王子健, 周思羽. 基于LADRC的舰载V/STOL飞机短距起飞性能优化[J]. 航空学报, 2019, 40(6): 122772-122772.
[9]	张军徽, 佟安, 武娜, 刘应华. 太阳帆航天器在绕地轨道中的热诱发振动[J]. 航空学报, 2019, 40(11): 223135-223135.
[10]	刘为杰, 何帆, 凌忠伟. 2.4 m跨声速风洞流场预测自抗扰控制[J]. 航空学报, 2019, 40(11): 123154-123154.
[11]	董方酉, 孙青林, 张晓雷, 蒋玉新, 孙明玮, 陈增强. 基于死区补偿的氧调器平稳切换自抗扰控制[J]. 航空学报, 2018, 39(5): 321875-321875.
[12]	马振宇, 祝小平, 周洲. 一种方向舵-螺旋桨联用的全翼式太阳能无人机横航向控制方法[J]. 航空学报, 2018, 39(3): 321633-321633.
[13]	陶金, 孙青林, 檀盼龙, 邬婉楠, 陈增强, 贺应平. 翼伞系统在未知风场中的归航控制[J]. 航空学报, 2017, 38(5): 320523-320523.
[14]	王正玺, 张葆, 李贤涛, 张士涛, 马丙华. 航空光电稳定平台高性能摩擦力补偿方案[J]. 航空学报, 2017, 38(12): 321350-321350.
[15]	谢振伟, 郭迎清, 姜彩虹, 田飞龙, 李睿超. 变循环发动机完全分布式控制[J]. 航空学报, 2016, 37(6): 1809-1818.