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精确定点归航翼伞控制系统的研究

李春 吕智慧 黄伟 沈超

中南大学学报(自然科学版)2012,Vol.43Issue(4):1331-1335,5.
中南大学学报(自然科学版)2012,Vol.43Issue(4):1331-1335,5.

精确定点归航翼伞控制系统的研究

Guidance navigation & control system for precision fix-point homing parafoil

李春 1吕智慧 1黄伟 1沈超1

作者信息

  • 1. 北京空间机电研究所,北京,100076
  • 折叠

摘要

Abstract

Using embedded navigation & control device, double-antenna GPS device, unwire data transporter and big moment direct current electromotor, navigation control software, landing point pre-setting software, remote control & communication software, GPS data converse software was designed independently. Precision fix-point homing parafoil control system which has two working modes of automatic homing and manual remote control was developed. In the automatic homing mode, system controls parafoil approaching the pre-setted target point. And in the manual remote control mode, ground operating person sends remote control instructions to operate parafoil returning using ground control computer. And the control system was validated by association test and load test, respectively. The result indicates that the control system our research provided fulfilled the demand of controllable parafoil fix-point homing.

关键词

精确定点/翼伞/GPS/归航

Key words

precision fix-point/ parafoil/ GPS/ homing

分类

信息技术与安全科学

引用本文复制引用

李春,吕智慧,黄伟,沈超..精确定点归航翼伞控制系统的研究[J].中南大学学报(自然科学版),2012,43(4):1331-1335,5.

基金项目

国家“十二五”民用航天技术预先研究项目(D010101) (D010101)

中南大学学报(自然科学版)

OA北大核心CSCDCSTPCD

1672-7207

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