基于DSP的一体化PGK控制系统设计 |
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引用本文: | 杨世武,邓健辉,彭俊然,陈庆,李闯. 基于DSP的一体化PGK控制系统设计[J]. 计算机测量与控制, 2019, 27(3): 121-125 |
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作者姓名: | 杨世武 邓健辉 彭俊然 陈庆 李闯 |
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作者单位: | 华中科技大学电气与电子工程学院,武汉,430723;中国航天科技集团烽火机械,成都,611130 |
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基金项目: | 航天科技创新(天科研[2015]1133号研KJCX-JT-1601) |
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摘 要: | 弹载系统的一体化、模块化已成为趋势,据此提出利用DSP来实现精确制导组件(Precision Guidance Kit, PGK)一体化系统的控制,完成导弹的制导和控制任务,从而提高弹载系统的可靠性和导弹的作战能力;叙述了PGK控制系统中硬件与软件的设计过程,包括对控制模块、GPS接收机、地磁测量模块、无线装定模块等的设计和功能介绍,以及对软件工作流程和软件模块进行简要介绍;通过发射安装本PGK系统的修正弹进行飞行试验,GPS模块与地磁测量模块的测试结果表明该系统可以基本实现模块功能。
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关 键 词: | DSP PGK 精确制导 一体化 |
收稿时间: | 2018-09-21 |
修稿时间: | 2018-10-18 |
Design of Integrated PGK Control System Based on DSP |
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Abstract: | The integration and modularization of the missile-borne system has become a trend. Based on this, it is proposed to use DSP to realize the control of the Precision Guidance Kit (PGK) system and to complete the missile guidance and control tasks, in order to improve the reliability of the missile-borne system and the combat capability of the missile; the design process of hardware and software of the PGK control system is described, including the design and function introduction of the control module, GPS receiver, geomagnetic measurement module, wireless setting module, etc., as well as the software workflow and software modules. The flight test was carried out by launching the modified missile with the PGK, and the test results of the GPS module and the geomagnetic measurement module showed that the system can basically realize the module function. |
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Keywords: | DSP PGK Precision guidance Integration |
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