期刊文献+

基于dSPACE的微型核仿真验证系统 被引量:3

dSPACE-based micro core simulation system
下载PDF
导出
摘要 为验证微型核原理样机软/硬件实时性能,采用dSPACE实时仿真器建立以微型核为核心的实时仿真验证系统。针对搭建微型核实时仿真验证系统的要求,重点解决了如何用dSPACE仿真器模拟外部实时仿真环境,以及微型核CAN总线和dSPACE仿真器RS232串口之间数据转换的难题。在系统成功建立的基础上,进行了小卫星姿态控制全模式实时仿真,完成了对微型核实时软/硬件性能的测试。仿真结果证明了本仿真验证系统软/硬件结构的正确性。 To verify the performance of the software and hardware of micro core, a real-time simulation system based on micro core is established by using dSPACE simulation system. According to the requirements of building the real-time simulation system, some technical problems are solved, such as how to use dSPACE system to simulate exterior real-time simulation environments and the data transformation between CAN bus of micro core and serial RS232 of dSPACE. Then, after successfully building the real-time simulation system, the full-mode attitude control simulation is performed to test the real-time performance of software and hardware of micro core. The result of the simulation demonstrates the validity of the software and hardware architecture of this real-time simulation system.
出处 《系统工程与电子技术》 EI CSCD 北大核心 2007年第12期2149-2153,共5页 Systems Engineering and Electronics
基金 国家安全重大基础研究"973"项目基金资助课题(5131201)
关键词 卫星 DSPACE 微型核 串口模型 satellite dSPACE micro core serial model
  • 相关文献

参考文献8

  • 1DasA. Techsat21-space missions using collaborating constellations of satellites[C]//Utah State University. 12th AIAA/USU Conference on Small Satellites. Logan, Utah, 1998:1 -5.
  • 2Voss David L, Kirchoff A, Hagerman D P. TEST: A modular scientific nanosatellite[C]//Space Conference and Exhibit, San Diego California, 2004.
  • 3Rankin D, Kekez D D, Zee R E. The CanX-2 nanosatellite expanding the science abilities of nanosatellites[J]. Acta Astronautica, 2005,57:167- 174.
  • 4龚晓春,徐国栋,邢雷.应用于微型航天器的微型核技术[J].吉林大学学报(工学版),2006,36(5):772-777. 被引量:2
  • 5dSPACE Inc. dSPACE implementation guide[R]. Paderborn: dSPACE Inc , 2001.
  • 6朱承元,杨涤,翟坤.基于dSPACE的星载计算机外部实时仿真环境实现[J].系统仿真学报,2004,16(10):2298-2301. 被引量:6
  • 7杨旭,孙兆伟,朱承元,翟坤.基于dSPACE的卫星控制实时仿真系统设计[J].系统工程与电子技术,2005,27(2):335-339. 被引量:14
  • 8MATLAB Stateflow user' s guide [Z]. The Math Works Inc, 2001.

二级参考文献15

  • 1林来兴,张新邦.飞行仿真技术新的发展及其在航天领域中应用[J].计算机仿真,1996,13(1):13-20. 被引量:6
  • 2Jokic M D, Asokanthan S F. Tethered satellite system models for use in hardware-in-the-loop simulations [ A ]. AIAA/ASME/ASCE/AHS/ASCStructures, Structural Dynamics and Materials Conference, 2001, 3:1791- 1799.
  • 3dSPACE real-time interface (RTI and RTI-MP) implementation guide [Z]. dSPACE GmbH, 2001. 1 -76.
  • 4dSPACE ControlDesk experiment guide[Z]. dSPACE GmbH, 2001.
  • 5Jokic M.D, Asokanthan S F. Tethered satellite system models for use in hardware-in-the-loop simulations [C]. AIAA Structures, Structural Dynamics and Materials Conference, 2001, 3: 1791-1799.
  • 6MATLAB Stateflow User's Guide [Z]. The MathWorks, Inc.2001
  • 7Zahid S, Ayyaz N. An economical on-board computer for low-earth-orbit satellites [ J]. Students Conference, ISCON02 Proceedings IEEE 2002, 1 (16-17) :66-75.
  • 8Mcdermott S A, Jacobovits A, Yashiro H. Automotive electronics in space: combining the advantages of high reliability components with high production volume [ J ].Aerospace Conference Proceedings, 2002, 4: 1857-1869.
  • 9Dubourg V, Carayon J L, Danto P, et al. An innovative onboard computer for CNES microsatellites [ J ]. AIAA IEEE Dig Avionics Syst Conf Proc, 2002, 2: 9B21-9B211.
  • 10Gillespie T, Gamber T, Chun W. Enabling technologies for microspacecraft [ J ]. IEEE Aerospace Conference Proceedings, 2000, 4 : 15-21.

共引文献17

同被引文献20

  • 1朱承元,杨涤,翟坤.基于dSPACE的星载计算机外部实时仿真环境实现[J].系统仿真学报,2004,16(10):2298-2301. 被引量:6
  • 2刘淑芬,孙昕.CAN总线在卫星中的应用技术研究[J].航天控制,2004,22(6):79-83. 被引量:18
  • 3朱承元,杨涤,杨旭.卫星姿轨控实时仿真系统及串口通信建模[J].哈尔滨工业大学学报,2005,37(1):26-31. 被引量:4
  • 4杨旭,孙兆伟,朱承元,翟坤.基于dSPACE的卫星控制实时仿真系统设计[J].系统工程与电子技术,2005,27(2):335-339. 被引量:14
  • 5Marko B,Monte M.Hardware in-the-loop simulation of aerodynamic objects[C].AIAA2007-6465,AIAA Modeling and Simulation Technologies Conference and Exhibit,South Carolina,USA,August 20-23,2007.
  • 6Guy W,Ken L,Richard W.Modeling and simulation technologies:reconfigurable flight simulators in modeling and simulation[C].AIAA2004-5459,AIAA Modeling and Simulation Technologies Conference and Exhibit,Rhode Island,USA,August 16-19,2004.
  • 7Farhan A F,Thanh L V.Mathematical models for a missile autopilot design[R].Australia:Weapons Systems Division Systems Sciences Laboratory,August 2002.
  • 8dSPACE GmbH.dSPACE realtime interface (RTI and RTI-MP) implementation guide[M].Paderborn:dSPACE GmbH Technology,2004.
  • 9dSPACE GmbH.Controldesk:hardware installation and configuration reference[M].Paderborn:dSPACE GmbH Technology,2004.
  • 10KIM B, VELENIS E, KRIENGSIRI P, et al. Designing a low-cost spacecraft simulator [ J ]. IEEE Control Sys- tems Magazine, 2003, 23 (4) :26 - 37.

引证文献3

二级引证文献9

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