Errors Analysis of Rendezvous and Docking Training Simulation

您当前的位置：

首页 >

文章列表页 >

Errors Analysis of Rendezvous and Docking Training Simulation

更新时间：2025-07-09

- Errors Analysis of Rendezvous and Docking Training Simulation
- Vol. 46, Issue 10, Pages: 127-132(2012)
- 作者机构：
  
  1. 西安交通大学电子与信息工程学院,西安,710049
  2. 中国航天员科研训练中心,北京,100094
- 作者简介：
- 基金信息：
- DOI：
  CLC： V526
- Online First：10 October 2012，
  
  Published：2012
- 稿件说明：
移动端阅览
Errors Analysis of Rendezvous and Docking Training Simulation[J]. 2012, 46(10): 127-132.
DOI：

Errors Analysis of Rendezvous and Docking Training Simulation[J]. 2012, 46(10): 127-132. DOI：

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.

Abstract

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.

关键词

Keywords

references

张柏楠. 航天器交会对接任务分析与设计[M]. 北京: 科学出版社, 2011: 1-47.

STEPHENS J, VOS G, BILIMORIA K, et al. Orion handling qualities during ISS proximity operations and docking[C]∥AIAA Guidance, Navigation, and Control Conference. Reston, USA: AIAA, 2011: 6261.

PADFIELD G, WHITE M. Measuring simulation fidelity through an adaptive pilot model[J]. Aerospace Science and Technology, 2005, 9: 400-408.

GELLER D. Linear covariance techniques for orbital rendezvous analysis and autonomous onboard mission planning[J]. Journal of Guidance, Control, and Dynamics, 2006, 29(6): 1404-1414.

SULLIVAN J, LEE A, GROVER M. Rendezvous and docking sensor and effector system design considerations for the lunar lander Altair[C]∥AIAA Guidance, Navigation, and Control Conference. Reston, USA: AIAA, 2010: 7723.

BILIMORIAB K, MUELLER E, FORST C. Handling qualities evaluation of pilot tools for spacecraft docking in earth orbit[J]. Journal of Spacecraft and Rockets, 2011, 48(5): 846-855.

BAILEY R, JACKSON B, GOODRICH K. Initial investigation of reaction control system design on spacecraft handling qualities for earth orbit docking[C]∥AIAA Atmospheric Flight Mechanics Conference and Exhibit. Reston, USA: AIAA, 2008: 6553.

LIANG Libo, LUO Yazhong. Rendezvous-phasing errors propagation using quasi-linearization method[C]∥AIAA Guidance, Navigation, and Control Conference. Reston, USA: AIAA, 2010: 7594.

LEE D. Guidance, navigation and control system for autonomous proximity operations and docking of spacecraft[D]. Rolla, Missouri, USA: Missouri University of Science and Technology, 2009: 21-32.

WOFFINDEN D, GELLER D. Relative angles-only navigation and pose estimation for autonomous orbital rendezvous[J]. Journal of Guidance, Control and Dynamics, 2007, 30(5): 1455-1469.

杨进, 姜国华, 晁建刚. 基于靶标图像的航天员手控对接方法[J]. 宇航学报, 2010, 31(5): 1398-1404.

YANG Jin, JIANG Guohua, CHAO Jiangang. A cross drone image-based manual control rendezvous and docking method[J].Journal of Astronautics, 2010, 31(5): 1398-1404.

XU Ruifeng. Real-time realistic rendering and high dynamic range image display and compression [D]. Orlando, Florida, USA: University of Central Florida Orlando, 2005: 32-47.

Views

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Error Analysis and Compensation of Linear Structured Light Scanning Probes

Measurement Alignment Error Analysis for In-Plane Motion of a Precision Levitation Stage

Prophet+: an Extended Multicore Simulator for Speculative Multithreading

Influence of Numerical Integration on Error of Ultrasonic Flowmeter

Influence of Structural Parameters on the Summer Operational Characteristics of a Three-Tower-in-One Indirect Air-Cooling System

Related Author

陈磊

郭俊杰

李兵

蒋庄德

丁建军

毛军红

伍宏亮

王旭昊

Related Institution

State Key Laboratory for Manufacturing Systems Engineering, Xi'an Jiaotong University

Theory of Lubrication and Bearing Institute, Xi'an Jiaotong University

Department of Computer Science and Technology, Xi'an Jiaotong University

MOE Key Laboratory of Thermo-Fluid Science and Engineering, Xi'an Jiaotong University

⁰