航天器惯性及其组合导航技术发展现状

doi:10.3969/j.issn.1674-5558.2020.h4.007

摘要/Abstract

摘要： 航天器是在地球大气层以外运动的飞行器,也包括部分从宇宙空间返回地球的飞行器。在航天器的飞行过程中,惯性敏感器是实现航天器姿态确定、速度变化测量的关键敏感器之一。随着航天器任务的不断扩展,航天器对惯性器件的使用日趋复杂,高精度定姿、惯性导航、组合导航等技术在应用深度和广度上不断发展。以此为背景,对航天器惯性技术的发展脉络进行了全面的梳理和总结,包括惯性技术的使用方式、技术现状以及未来发展等几个方面的内容。

关键词: 航天器, 惯性技术, 组合导航

Abstract: Spacecraft is a vehicle fighting in extra-atmosphere, and also includes some earth reentry vehicles. During flight, inertial technology is critical important to assist the spacecraft to determine its attitude and velocity increment. As the missions become more complex, the application fields of inertial sensors expand rapidly and cover high precision attitude determination, inertial navigation, integrated navigation, et al. On this background, the development context of inertial technology for spacecraft is discussed in this paper, including the category of usage, present situation and future needs.

Key words: spacecraft, inertial technology, integrated navigation

中图分类号:

V448.21

袁利, 李骥. 航天器惯性及其组合导航技术发展现状[J]. 导航与控制, 2020, 19(4/5): 53-63.

YUAN Li, LI Ji. The Development of Inertial and Integrated Navigation Technology for Spacecraft[J]. Navigation and Control, 2020, 19(4/5): 53-63.

参考文献

[1] 袁利, 黄煌. 空间飞行器智能自主控制技术现状与发展思考[J]. 空间控制技术与应用, 2019, 45(4): 7-18.
YUAN Li, HUANG Huang. Current trends of spacecraft intelligent autonomous control[J]. Aerospace Control and Application, 2019, 45(4): 7-18.
[2] Lam Q M, Hunt T,Sanneman P, et al. Analysis and design of a fifteen state stellar inertial attitude determination system[C]. AIAA Guidance, Navigation, and Control Conference and Exhibit, 2003.
[3] Madden M. GeoEye-1, the world's highest resolution commercial satellite[C]. IEEE Conference on Lasers and Electro-Optics, 2009.
[4] GeoEye-1[EB/OL]. http://directory.eoportal.org/web/eoportal/satellite-missions/g/geoeye-1.
[5] WorldView-3[EB/OL]. http://directory.eoportal.org/web/eoportal/satellite-missions/v-w-x-y-z/worldview-3.
[6] WorldView-4(formerly GeoEye-2) [EB/OL]. http://directory.eoportal.org/web/eoportal/satellite-missions/v-w-x-y-z/worldview-4.
[7] 张承钰, 袁利, 王立, 等. 空间光学敏感器像素位置精确测量技术发展现状[J]. 空间控制技术与应用, 2019, 45(2): 11-17.
ZHANG Cheng-yu, YUAN Li, WANG Li, et al. Current situation of pixel position accurate measurement technique for spatial optical sensor[J]. Aerospace Control and Application, 2019, 45(2): 11-17.
[8] 卢欣, 武延鹏, 钟红军, 等. 星敏感器低频误差分析[J]. 空间控制技术与应用, 2014, 40(2): 1-7.
LU Xin, WU Yan-peng, ZHONG Hong-jun, et al. Low frequency error analysis of star sensor[J]. Aerospace Control and Application, 2014, 40(2): 1-7
[9] 霍德聪, 黄琳, 李岩, 等. 星敏感器在轨测量误差分析[J]. 遥感学报, 2012, 16(z1): 57-60.
HUO De-cong, HUANG Lin, LI Yan, et al. An analytical method of star tracker measurement errors[J]. Journal of Remote Sensing, 2012, 16(z1): 57-60.
[10] 熊凯, 宗红, 汤亮. 星敏感器低频误差在轨校准方法研究[J]. 空间控制技术与应用, 2014, 40(3): 8-13.
XIONG Kai, ZONG Hong, TANG Liang. On star sensor low frequency error in-orbit calibration method[J]. Aerospace Control and Application, 2014, 40(3): 8-13.
[11] 庞博, 李果, 黎康, 等. 一种基于地标的星敏感器低频误差在轨校正方法[J]. 航天器工程, 2018, 27(3): 79-85.
PANG Bo, LI Guo, LI Kang, et al. On-orbit calibration method of star sensor's low frequency error based on landmark[J]. Spacecraft Engineering, 2018, 27(3): 79-85.
[12] 赵琳, 谢瑞达, 刘源, 等. 星敏感器低频误差与陀螺漂移离线校正方法[J]. 航空学报, 2017, 38(5): 197-210.
ZHAO Lin, XIE Rui-da, LIU Yuan, et al. Offline calibration method of low frequency error of star sensor and gyroscope drift[J]. Acta Aeronautica ET Astronautica Sinica, 2017, 38(5): 197-210.
[13] Savage P G.Strapdown inertial navigation integration algorithm design part 1: attitude algorithms[J]. Journal of Guidance, Control and Dynamics, 1998, 21(1): 19-28.
[14] Savage P G.Strapdown inertial navigation integration algorithm design part 2: velocity and position algorithms[J]. Journal of Guidance, Control and Dynamics, 1998, 21(2): 208-221.
[15] 李骥, 张洪华, 赵宇, 等. 嫦娥三号着陆器的陀螺在轨标定[J]. 中国科学: 技术科学, 2014, 44(6): 582-588.
LI Ji, ZHANG Hong-hua, ZHAO Yu, et al. In-flight calibration of the gyros of the Chang'E-3 lunar lander[J]. Scientia Sinica(Technologica), 2014, 44(6): 582-588.
[16] Li J, Wang D Y. Autonomous positioning and orientating for lunar launch[C]. 62^nd International Astronautical Congress, 2011
[17] 高阳, 王猛, 刘蕾, 等. 基于高轨航天器的GNSS接收机技术[J]. 中国空间科学技术, 2017, 37(3): 101-109.
GAO Yang, WANG Meng, LIU Lei, et al. GNSS receiver techniques based on high earth orbit spacecraft[J]. Chinese Space Science and Technology, 2017, 37(3): 101-109.
[18] Kriegsman B A. Radar-update inertial navigation of a continuously-powered space vehicle[J]. IEEE Transactions on Aerospace and Electronic Systems, 1966, AES-2(4): 549-565.
[19] Eichler J. A performance study of the lunar module's landing radar system[J]. Journal of Spacecraft and Rockets, 1968, 5(9): 1016-1022.
[20] 张洪华, 李骥, 关轶峰, 等. 嫦娥三号着陆器动力下降的自主导航[J]. 控制理论与应用, 2014, 31(12): 1686-1694.
ZHANG Hong-hua, LI Ji, GUAN Yi-feng, et al. Autonomous navigation for powered descent phase of Chang'E-3 lunar lander[J]. Control Theory & Applications, 2014, 31(12): 1686-1694.
[21] Ely T A,Chau A H. Radar altimetry and velocimetry for inertial navigation: a lunar landing example[C]. AAS/AIAA Astrodynamics Specialist Conference, 2011: 2041-2060.
[22] Ning X L, Gui M Z, Fang J C, et al. A novel autonomous celestial navigation method using solar oscillation time delay measurement[J]. IEEE Transactions on Aerospace and Electronic Systems, 2018, 54(3): 1392-1403.
[23] Lee A Y, Ely T A, Sostaric R R, et al. Preliminary design of the guidance, navigation, and control system of the Altair lunar lander[C]. AIAA Guidance, Navigation, and Control Conference, 2010.
[24] 张洪华, 关轶峰, 程铭, 等. 嫦娥四号着陆器制导导航与控制系统[J]. 中国科学: 技术科学, 2019, 49(12): 1418-1428.
ZHANG Hong-hua, GUAN Yi-feng, CHENG Ming, et al. Guidance navigation and control for Chang'E-4 lander[J]. Scientia Sinica(Technologica), 2019, 49(12): 1418-1428.
[25] Li R S, Needelman D, Fowell R, et al. Reusable stellar inertial attitude determination(SIAD) design for spacecraft guidance, navigation & control[C]. AIAA Guidance, Navigation, and Control Conference and Exhibit, 2005.
[26] 江城, 张嵘. 美国Micro-PNT发展综述[C]. 第六届中国卫星导航学术年会, 2015.
JIANG Cheng, ZHANG Rong. Overview on American micro-PNT development[C]. 6^th China Satellite Navigation Conference, 2015.
[27] Richeson J A, Pines D J. GPS denied inertial navigation using gravity gradiometry[C]. AIAA Guidance, Naviga-tion and Control Conference and Exhibit, 2007.
[28] 窦爱萍, 李鹏, 张磊, 等. 全源自适应导航技术研究[J]. 航空计算技术, 2018, 48(5): 318-324.
DOU Ai-ping, LI Peng, ZHANG Lei, et al, Research on navigation technology with all sources adaptive[J]. Aeronautical Computing Technique, 2018, 48(5): 318-324.
[29] Kaidy J, Criss T, Dong C, et al. Robotic lunar lander guidance, navigation and control concept and analysis[C]. AAS/AIAA Astrodynamics Specialist Conference, 2011: 69-87.
[30] Ely T A,Heyne M, Riedel J E. Altair navigation performance during translunar cruise, lunar orbit, descent, and landing[J]. Journal of Spacecraft and rockets, 2012, 49(2): 295-317.
[31] Riedel J E, Vaughan A T, Werner R A, et al. Opticalnavigation plan and strategy for the lunar lander Altair; OpNav for lunar and other crewed and robotic exploration applications[C]. AIAA Guidance, Navigation, and Control Conference, 2010.
[32] Nelessen A, Sackier C, Clark I, et al, Mars 2020 entry, descent, and landing system overview[C]. IEEE Aeros-pace Conference, 2019.
[33] Lightsey E G, Mogensen A E, Burkhart P D, et al. Real-time navigation for Mars missions using the Mars Network[J]. Journal of Spacecraft and Rockets, 2008, 45(3): 519-533.
[34] Bell D J, Cesarone R, Ely T A, et al. Mars network: a Mars orbiting communications and navigation satellite constellation[C]. IEEE Aerospace Conference Proceedings, 2000: 75-88.
[35] 崔平远, 窦强, 高艾. 火星大气进入段通信 “黑障” 问题研究综述[J]. 宇航学报, 2014, 35(1): 1-12.
CUI Ping-yuan, DOU Qiang, GAO Ai. Review of communication blackout problems encountered during Mars entry phase[J]. Journal of Astronautics, 2014, 35(1): 1-12.
[36] 夏元清. 火星探测器进入、下降与着陆过程的导航、制导与控制——“恐怖”七分钟[M]. 北京: 科学出版社, 2018.
XIA Yuan-qing. Navigation, guidance and control for the Mars entry, descent, and landing phase [M]. Beijing: Science Press, 2018.
[37] Morabito D D. The spacecraft communications blackout problem encountered during passage or entry of planetary atmospheres[R]. Pasadena: Jet Propulsion Laboratory, 2002.
[38] Bahm C, Baumann E, Martin J, et al. The X-43A Hyper-X Mach 7 flight 2 guidance, navigation, and control overview and flight test results[C]. AIAA/CIRA 13^th International Space Planes and Hypersonic Systems and Technologies, 2005.
[39] Karlgaard C D, Beck R E, O'Keefe S A, et al. Mars entry atmospheric data system modeling and algorithm development[C]. 41^st AIAA Thermophysics Conference, 2009.
[40] Gazarik M J, Wright M J, Little A, et al. Overview of the MEDLI project[C]. IEEE Aerospace Conference, 2008.
[41] 常国宾, 李胜全. 惯性技术视角下动态重力测量技术评述(三): 惯性导航与重力测量的融合[J]. 海洋测绘, 2014, 34(5): 7-12.
CHANG Guo-bin, LI Sheng-quan. Overview on dynamic gravimetry in the perspective of inertial technology, part III: the fusion of inertial navigation and gravimetry[J]. Hydrographic Surveying and Charting, 2014, 34(5): 7-12.