期刊文献+

基于DSP的旋转弹用微小型导航系统设计

Design of Micro-navigation for Spinning Projectile based on DSP
下载PDF
导出
摘要 在无陀螺捷联惯导系统中,针对旋转弹体积小、功耗大、采样频率高、姿态变化快、解算周期短等问题。为满足旋转弹对其导航计算机的严格要求,提出了一种基于DSP的旋转弹用微小型导航系统设计,首先叙述了系统的总体方案设计,接着重点介绍了系统各模块的软硬件设计。本设计在硬件上节省了系统的体积和功耗,软件设计上节省了解算周期。 In the gyroscope-free strapdown inertial navigation system,the spinning projectile has little volume,low power,high sampling rate,high roll angular velocity and short resolving time.To meet the strict requirements of the spinning projectile to its navigation computer,adesign of micro-navigation for spinning projectile based on DSP is proposed.The article first narrated the processor of system project design and chip selection,summarized structure and character of DSP.Then it focused on introduction of hardware and software design of GFSINS.This design saves the volume and power in the hardware and period of resolving in the software.
出处 《火力与指挥控制》 CSCD 北大核心 2010年第6期170-172,共3页 Fire Control & Command Control
关键词 无陀螺捷联惯导系统 旋转弹 DSP gyroscope-free strapdown inertial navigation system spinning projectile DSP
  • 相关文献

参考文献6

  • 1曹咏弘,祖静,林祖森.无陀螺捷联惯导系统综述[J].测试技术学报,2004,18(3):269-273. 被引量:37
  • 2TMS320C6000 CPU and Instruction Set Reference Guide [ S ]. SPRU189, Texas Instruments Incorporated, 2000.
  • 3张萌 马铁华 范锦彪等.旋转弹用微小型导航计算机设计.中北大学学报,2007,28:77-80.
  • 4赵倩,马铁华,范锦彪.基于DSP的无陀螺捷联惯导系统设计[J].电子测试,2008,19(8):67-70. 被引量:2
  • 5TMS320C6000 Peripherals Reference Guide. Texas Instruments Incorporated[S]. 2001.
  • 6TMS320C6000 Technical Brief. Texas Instruments Incorporated [S]. 1999.

二级参考文献26

  • 1曹咏弘,祖静,林祖森.无陀螺捷联惯导系统综述[J].测试技术学报,2004,18(3):269-273. 被引量:37
  • 2Merhav S J. A Non-gyroscopic Inertial Measurement Uint[J]. Journal of Guidance and Control, 1982, 5(3): 227-235.
  • 3Algrain M C. Accelerometer-Based Platform Stabilization[J]. SPIE Acquisition Tracking and Pointing, 1991, 1482: 367-382.
  • 4Chen J H, Lee S C, Daniel B. Gyroscope Free Strap-down Inertial Measurement Unit by Six Linear Accelerometers[J]. Journal of Guidance Control and Dynamics, 1994, 17(2): 286-290.
  • 5Corey V B. Measuring Angular Acceleration with Linear Acceleration[J]. Control Engineering, 1962, (2): 79-80.
  • 6Lee S C, Huang Y C. Innovative estimation method with measurement likelihood for all-accelerometer type inertial navigation system[J].IEEE Trans. on AES. 2002, 38(1): 339-346.
  • 7Krishnan V. Measurement of Angular Velocity and Linear Acceleration Using Linear Accelerometers[J]. Journal of The Franklin Institute, 1965, 280(4): 307-315.
  • 8Schuler A R. Measuring Rotational Motion with Linear Accelerometers[J]. IEEE Trans onAES, 1967, 3(3): 465-472.
  • 9Padgaonkar A J, Krieger K W, King A I. Measurement of Angular Acceleration of a Rigid Body Using Linear Acce-lerometers[J]. Journal of Applied Mechanics, 1975, 42(5): 552-556.
  • 10Lee S C, Cheng Y L. Innovative Estimation Method with Own-ship Estimator for an All accelerometer-type Inertial Navigation System[J]. International J of Systems Science, 1999, 30(12): 1259-1266.

共引文献37

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