基于燃料最优解的火星精确着陆制导策略研究

姓名
邮箱
手机号码
标题
留言内容
验证码

doi:10.15982/j.issn.2095-7777.2015.01.009

1.
哈尔滨工业大学控制科学与工程系, 哈尔滨 150001
2.
哈尔滨工业大学深空探测基础研究中心, 哈尔滨 150001

基金项目:国家973计划项目(2012CB720000) ;国家自然科学基金资助项目(61403103);中国博士后科学基金资助项目(2014M550195)

Mars Precision Landing Guidance Strategy based on Fuel Optimal Solutions

1.
Department of Control Science and Engineering, Harbin Institute of Technology, Harbin 150001, China
2.
Deep Space Exploration Research Center, Harbin Institute of Technology, Harbin 150001, China

摘要:针对火星着陆任务高实时性和低燃耗的需求,提出了一种新的基于开环燃料最优解的精确着陆制导策略。通过分析开环燃料最优解特性,设计了利用发动机推力幅值切换处的状态作为路径点结合最优线性制导律进行分段制导的制导策略,在无需存储全部燃料最优轨迹的前提下,实现具有近燃料最优特性的着陆任务,节省了大量的存储空间。同时详细讨论了包括全局燃料最优解获取、路径点提取、路径点拟合等一系列关键问题,并通过典型火星着陆场景的大量数学仿真验证了所提出策略的可行性和优越性。
- 精确着陆/
- 动力下降/
- 路径点/
- 最优制导/
- 轨迹跟踪
Abstract:In order to satisfy real time and low fuel consumption requirements of Mars descent phrase, a new Mars precision landing guidance strategy was proposed based on fuel optimal solutions. Based on the characteristic analysis of the open loop fuel optimal solutions, states corresponding to thruster force magnitude switching time are directly selected as intermediate waypoints, and then a linear guidance algorithm was implemented in each segments to achieve fuel optimal performance. Several key problems, including the computation of global fuel optimal solution, waypoint selection, waypoint fitting, and derivation of linear guidance algorithm, were discussed in details, and the feasibility and superiority of the proposed strategy have been evaluated through a variety of typical Mars landing scenarios.
- precision landing/
- dynamic descent/
- waypoint/
- optimal guidance/
- trajectory tracking

[1]	Braun R D, Manning R M. Mars exploration entry, descent and landing challenges[J]. Journal of Spacecraft and Rockets, 2007,44(2):310-323.
[2]	安德鲁·鲍尔等著. 行星着陆器和进入探测器[M].殷前根等译.北京:中国宇航出版社,2010.[ Ball A J,et al. Planetary landers and entry probes[M]. Translator, Yin Q G, et al. Beijing: China Astronautic Publishing House, 2010.]
[3]	D'Souza C N. An optimal guidance law for planetary landing[C]//Proceedings of the AIAA Guidance, Navigation and Control Conference. New Orleans:[s.n.], 1997.
[4]	Steinfeldt B A, Grant M J, Matz D A,et al. Guidance, navigation, and control system performance trades for Mars pinpoint landing[J]. Journal of Spacecraft and Rockets, 2010,47(1):188-198.
[5]	Najson F, Mease K D. Computationally inexpensive guidance algorithm for fuel-efficient terminal descent[J]. Journal of Guidance, Control, and Dynamics, 2006,29(4):955-964.
[6]	Furfaro R, Selnick S, Cupples M L, et al. Non-linear sliding guidance algorithms for precision Lunar landing[C]//21st AAS/AIAA Space Flight Mechanics Meeting. Louisiana, New Orleans:[s.n.], 2011:945-964.
[7]	Gaudet B, Furfaro R. Adaptive pinpoint and fuel efficient Mars landing using reinforcement learning[C]//22ed AAS/AIAA Space Flight Mechanics Meeting. Charleston, South Carolina:[s.n.], 2012:1309-1328.
[8]	Guo Y, Hawkins M, Wie B. Applications of generalized zero-effort-miss / zero-effort-velocity feedback guidance algorithm[J]. Journal of Guidance, Control and Dynamics, 2013,36(3):810-820.
[9]	Rutishauser D K, Epp C D, Robertson E A. Free-flight terrestrial rocket lander demonstration for NASA's autonomous landing and Hazard avoidance technology (ALHAT) system[C]//AIAA SPACE 2012 Conference & Exposition. Pasadena, California:[s.n.], 2012.
[10]	Acikmese B, Ploen S R. Convex programming approach to powered descent guidance for Mars landing[J]. Journal of Guidance, Control, and Dynamics, 2007,30(5):1353-1366.
[11]	Acikmese B, Blackmore L. Lossless convexification of a class of optimal control problems with non-convex control constraints[J]. Automatica, 2011,47(2):341-347.
[12]	Sostaric R R, Rea J R. Powered descent guidance methods for the Moon and Mars[C]//AIAA Guidance, Navigation, and Control Conference and Exhibit. San Francisco, California:[s.n.], 2005.
[13]	Shen H J, Seywald H, Powell R W. Desensitizing the minimum-fuel powered descent for Mars pinpoint landing[J]. Journal of Guidance, Control, and Dynamics, 2010,33(1):108-115.
[14]	Brian Kent Birge III. A computational intelligence approach to the Mars precision landing problem[D]. PhD dissertation of North Carolina State University, 2008.
[15]	Liu R, Li S, Chen X, et al. Powered-descent trajectory optimization scheme for Marslanding[J]. Advances in Space Research, 2013, 52(11):1888-1901.
[16]	Singh G, SanMartin A M, Wong E C. Guidance and control design for powered descent and landing on Mars[C]//IEEE Aerospace Conference. [S.l.]: IEEE, 2007:1-8.
[17]	Cui P Y, Gao A, Cui H T. Receding Horizon-based dual control strategy for pinpoint planetary landing[J]. Transactions of the Japan Society for Aeronautical and Space Sciences, 2012,55(4):222-228.
[18]	Li M D, Jing W X, Macdonald M,et al. Adaptive backstepping control for optimal descent with embedded autonomy[J]. Aerospace Science and Technology, 2011,15(7):589-594.
[19]	Guo Y, Hawkins M, and Wie B. Waypoint-optimized zero-effort-miss/zero-effort-velocity feedback guidance for Mars landing[J]. Journal of Guidance, Control, and Dynamics, 2013,36(3):799-809.

[1]	李明翔, 泮斌峰.行星着陆动力下降轨迹优化的中心差分凸化方法. 深空探测学报(中英文）, 2021, 8(2): 171-181.doi:10.15982/j.issn.2096-9287.2021.20200079
[2]	滕锐, 韩宏伟, 乔栋.火星探测最优离轨制导方法研究. 深空探测学报(中英文）, 2020, 7(2): 184-190.doi:10.15982/j.issn.2095-7777.2020.20190315001
[3]	冀红霞, 宗红, 黄翔宇.基于改进预测滤波的小天体精确着陆自主导航方法研究. 深空探测学报(中英文）, 2019, 6(3): 284-292.doi:10.15982/j.issn.2095-7777.2019.03.013
[4]	柯森锎, 李爽, 肖东东, 王卫华, 聂钦博.基于高斯伪谱法的火星表面上升燃耗最优轨迹设计. 深空探测学报(中英文）, 2018, 5(3): 269-275.doi:10.15982/j.issn.2095-7777.2018.6.009
[5]	郝万宏, 董光亮, 李海涛, 王宏, 樊敏, 周欢, 徐得珍.火星大气进入下降着陆段测控通信关键技术研究. 深空探测学报(中英文）, 2018, 5(5): 426-434.doi:10.15982/j.issn.2095-7777.2018.05.004
[6]	崔平远, 葛丹桐.一种行星安全着陆点综合评估方法. 深空探测学报(中英文）, 2016, 3(4): 363-369.doi:10.15982/j.issn.2095-7777.2016.04.008
[7]	葛丹桐, 崔平远.地外天体着陆点选择综述与展望. 深空探测学报(中英文）, 2016, 3(3): 197-203.doi:10.15982/j.issn.2095-7777.2016.03.001
[8]	袁旭, 朱圣英.基于伪谱法的小天体最优下降轨迹优化方法. 深空探测学报(中英文）, 2016, 3(1): 51-55.doi:10.15982/j.issn.2095-7777.2016.01.008
[9]	徐超, 王大轶, 黄翔宇.基于陆标图像的火星精确着陆自主导航方法研究. 深空探测学报(中英文）, 2016, 3(2): 150-155.doi:10.15982/j.issn.2095-7777.2016.02.009
[10]	王汀, 郭延宁, 张瑶, 马广富.基于模型预测控制的多约束火星精确着陆制导律研究. 深空探测学报(中英文）, 2016, 3(4): 377-383.doi:10.15982/j.issn.2095-7777.2016.04.010
[11]	江秀强, 陶婷, 杨威, 李爽.附着小天体的最优制导控制方法. 深空探测学报(中英文）, 2015, 2(1): 53-60.doi:10.15982/j.issn.2095-7777.2015.01.008
[12]	秦同, 朱圣英, 崔平远.火星软着陆能量最优制导律转移能力分析. 深空探测学报(中英文）, 2015, 2(3): 218-223.doi:10.15982/j.issn.2095-7777.2015.03.005
[13]	韩松涛, 唐歌实, 曹建峰, 陈略, 任天鹏, 王美.面向"CE-3号"软着陆过程的深空网干涉测量技术. 深空探测学报(中英文）, 2015, 2(2): 120-124.doi:10.15982/j.issn.2095-7777.2015.02.003
[14]	李爽, 陶婷, 江秀强, 张树瑜, 周杰.月球软着陆动力下降制导控制技术综述与展望. 深空探测学报(中英文）, 2015, 2(2): 111-119.doi:10.15982/j.issn.2095-7777.2015.02.002
[15]	黄翔宇, 张洪华, 王大铁, 李骥, 关软峰, 王鹏基.“嫦娥三号”探测器软着陆自主导航与制导技术. 深空探测学报(中英文）, 2014, 1(1): 52-59.
[16]	AlexanderGUSEV, 孟治国, 平劲松, NataliaPETROVA, HideoHANADA.多层月球模型的自转动力学与着陆探测. 深空探测学报(中英文）, 2014, 1(3): 175-180.doi:10.15982/j.issn.2095-7777.2014.03.002
[17]	张大鹏, 雷勇军.深空探测返回舱着陆冲击动力学分析. 深空探测学报(中英文）, 2014, 1(2): 150-155.
[18]	袁旭, 朱圣英, 乔栋, 崔平远.小天体着陆动力学参数不确定性影响分析. 深空探测学报(中英文）, 2014, 1(2): 134-139.
[19]	魏若岩, 阮晓钢, 庞涛, OuattaraSIE, 武旋, 肖尧.小天体软着陆中的地面特征区域提取与跟踪算法. 深空探测学报(中英文）, 2014, 1(4): 308-314.doi:10.15982/j.issn.2095-7777.2014.04.011
[20]	吴超, 赵振华, 杨俊, 李世华, 郭雷.基于约束预测控制的火星大气进入轨迹跟踪. 深空探测学报(中英文）, 2014, 1(2): 128-133.

点击查看大图

计量

文章访问数:2744
HTML全文浏览量:42
PDF下载量:1949
被引次数:0

留言板

基于燃料最优解的火星精确着陆制导策略研究

doi:10.15982/j.issn.2095-7777.2015.01.009

Mars Precision Landing Guidance Strategy based on Fuel Optimal Solutions

计量

基于燃料最优解的火星精确着陆制导策略研究

doi:10.15982/j.issn.2095-7777.2015.01.009

1. 哈尔滨工业大学控制科学与工程系, 哈尔滨 150001
2. 哈尔滨工业大学深空探测基础研究中心, 哈尔滨 150001

English Abstract

Mars Precision Landing Guidance Strategy based on Fuel Optimal Solutions

1. Department of Control Science and Engineering, Harbin Institute of Technology, Harbin 150001, China
2. Deep Space Exploration Research Center, Harbin Institute of Technology, Harbin 150001, China

全文HTML

目录

留言板

基于燃料最优解的火星精确着陆制导策略研究

doi:10.15982/j.issn.2095-7777.2015.01.009

Mars Precision Landing Guidance Strategy based on Fuel Optimal Solutions

计量

出版历程

基于燃料最优解的火星精确着陆制导策略研究

doi:10.15982/j.issn.2095-7777.2015.01.009

1. 哈尔滨工业大学 控制科学与工程系, 哈尔滨 1500012. 哈尔滨工业大学 深空探测基础研究中心, 哈尔滨 150001

English Abstract

Mars Precision Landing Guidance Strategy based on Fuel Optimal Solutions

1. Department of Control Science and Engineering, Harbin Institute of Technology, Harbin 150001, China2. Deep Space Exploration Research Center, Harbin Institute of Technology, Harbin 150001, China

全文HTML

目录

1. 哈尔滨工业大学控制科学与工程系, 哈尔滨 150001
2. 哈尔滨工业大学深空探测基础研究中心, 哈尔滨 150001

1. Department of Control Science and Engineering, Harbin Institute of Technology, Harbin 150001, China
2. Deep Space Exploration Research Center, Harbin Institute of Technology, Harbin 150001, China