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Control System in Missiles for Whole-Trajectory-Controlled Trajectory Correction Projectile Based on DSP

Zhang Zhian Chen Jun Lei Xiaoyun

南京航空航天大学学报(英文版)2014,Vol.31Issue(3):325-330,6.
南京航空航天大学学报(英文版)2014,Vol.31Issue(3):325-330,6.

Control System in Missiles for Whole-Trajectory-Controlled Trajectory Correction Projectile Based on DSP

Control System in Missiles for Whole-Trajectory-Controlled Trajectory Correction Projectile Based on DSP

Zhang Zhian 1Chen Jun 2Lei Xiaoyun1

作者信息

  • 1. ZNDY of Ministerial Key Laboratory, Nanjing University of Science and Technology, Nanjing, 210094, P.R.China
  • 2. The 28th Research Institute of China Electronics Technology Group Corporation, Nanjing, 210007, P.R.China
  • 折叠

摘要

关键词

trajectory correction projectile/digital signal processing (DSP)/GPS/entire course controlling/data storage

Key words

trajectory correction projectile/digital signal processing (DSP)/GPS/entire course controlling/data storage

分类

军事科技

引用本文复制引用

Zhang Zhian,Chen Jun,Lei Xiaoyun..Control System in Missiles for Whole-Trajectory-Controlled Trajectory Correction Projectile Based on DSP[J].南京航空航天大学学报(英文版),2014,31(3):325-330,6.

南京航空航天大学学报(英文版)

OACSCD

1005-1120

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