期刊文献+

交会对接航天员训练仿真误差分析 被引量:3

Errors Analysis of Rendezvous and Docking Training Simulation
下载PDF
导出
摘要 针对交会对接任务中地面训练仿真与实际飞行任务的天地一致性问题,研究了仿真中的关键误差并提出了对策.以航天员在回路中的感知为焦点,从仿真模型、视觉感知和操作感知等3个方面进行了误差特性分析研究.通过训练样本数据,讨论了自控/人控模式下训练仿真误差对航天员实飞操作品质的影响,提出了模型构建、过程修正和地面辨识等误差对策.试验结果表明,对策可行,时间延迟和操作精度响应仿真拉偏有效.误差分析和对策方法对训练模拟器研制和航天员训练有重要应用价值. Important errors existed in the consistency problem of ground training simulation with actual space flight in rendezvous and docking mission are investigated and countermeasures are put forward. Three characteristics of errors generated from simulation models, visual perception and operation perception are studied by focusing on astronauts' perception in the loop. The influence of training simulation errors in both autonomous docking mode and manual docking mode on astronaut's handling quality in real flight is analyzed in detail based on data of training samples, and approaches of model construction, midway-amending and identification are proposed. The statistic of simulation shows that the countermeasures are applicable, and the configurable bias of time delay and handling response in simulation are effective. The analyzing of simulation errors and countermeasures has a good application value for development of training simulator and astronauts; training.
出处 《西安交通大学学报》 EI CAS CSCD 北大核心 2012年第10期127-132,共6页 Journal of Xi'an Jiaotong University
关键词 交会对接 误差分析 训练仿真 模拟器 rendezvous and docking error analysis training simulation simulator
  • 相关文献

参考文献11

  • 1STEPHENS J,VOS G,BILIMORIA K,et al.Orionhandling qualities during ISS proximity operations anddocking[C] ∥AIAA Guidance,Navigation,and Con-trol Conference.Reston,USA:AIAA,2011:6261.
  • 2PADFIELD G,WHITE M.Measuring simulation fi-delity through an adaptive pilot model[J].AerospaceScience and Technology,2005,9:400-408.
  • 3GELLER D.Linear covariance techniques for orbitalrendezvous analysis and autonomous onboard missionplanning[J].Journal of Guidance,Control,and Dy-namics,2006,29(6):1404-1414.
  • 4SULLIVAN J,LEE A,GROVER M.Rendezvousand docking sensor and effector system design consid-erations for the lunar lander Altair[C] ∥AIAA Guid-ance,Navigation,and Control Conference.Reston,USA:AIAA,2010:7723.
  • 5BILIMORIAB K,MUELLER E,FORST C.Han-dling qualities evaluation of pilot tools for spacecraftdocking in earth orbit[J].Journal of Spacecraft andRockets,2011,48(5):846-855.
  • 6BAILEY R,JACKSON B,GOODRICH K.Initial in-vestigation of reaction control system design on space-craft handling qualities for earth orbit docking[C] ∥AIAA Atmospheric Flight Mechanics Conference andExhibit.Reston,USA:AIAA,2008:6553.
  • 7LIANG Libo,LUO Yazhong.Rendezvous-phasing er-rors propagation using quasi-linearization method[C] ∥AIAA Guidance,Navigation,and Control Conference.Reston,USA:AIAA,2010:7594.
  • 8LEE D.Guidance,navigation and control system forautonomous proximity operations and docking ofspacecraft[D].Rolla,Missouri,USA:Missouri Uni-versity of Science and Technology,2009:21-32.
  • 9WOFFINDEN D,GELLER D.Relative angles-onlynavigation and pose estimation for autonomous orbitalrendezvous[J].Journal of Guidance,Control and Dy-namics,2007,30(5):1455-1469.
  • 10杨进,姜国华,晁建刚.基于靶标图像的航天员手控交会对接方法[J].宇航学报,2010,31(5):1398-1404. 被引量:13

二级参考文献10

共引文献12

同被引文献16

  • 1李传庆,黄传红,孙福刚.一种分布式视景仿真软件系统通用框架[J].系统仿真学报,2013,25(S1):376-378. 被引量:8
  • 2潘晓宁.分布交互式实时三维飞行仿真平台的综合设计[J].计算机仿真,2007,24(1):285-290. 被引量:11
  • 3Brandon. Ground-to-flight handling qualities comparisons for a highperformance airplane [C]// NASA Langley Research CenterHampton. AIAA-95-3457-CP. USA: NASA, 1995.
  • 4David C Woffinden, David K Geller. Relative angles-onlynavigation and pose estimation for autonomous orbital rendezvous.Journal of Guidance, Control and Dynamic, 2007,30(5).
  • 5Daero Lee. Guidance. Navigation and control system for autonomousproximity operations and docking of spacecraft [D]. USA: MissouriUniversity of Science and Technology, 2009: 18-111.
  • 6Chi-Chang Johnny HO. Automatic spacecraft docking using computervision and nonlinear control Techniques [D]. USA: University ofMichigan, 1991.
  • 7Chi-Chang Johnny HO. Automatic spacecraft docking using computervision and nonlinear control Techniques [D]. USA: University ofMichigan, 1991..
  • 8朱仁淳.航天器交会对接技术[M].北京:国防工业出版社,2007:20-36.
  • 9杨乐平,朱彦伟,黄涣.航天器相对运动轨迹规划与控制[M].北京:国防工业出版社,2010: 5341.
  • 10John-Paul Stephens. Orion handling qualities during ISS proximityoperations and docking [C]// AIAA Guidance, Navigation, andControl Conference 08-11 August 2011, Portland, Oregon, USA.USA: AIAA.

引证文献3

二级引证文献1

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部