Software Design for Mini-type Ground Control Station of UAV
The guiding ideology and principle of GCS (Ground control Station) software design & development were proposed by analyzing the role of CGS in UA V (Unmanned Aerial Vehicle) systems. Firstly, established an abstract GCS software structure model of bi-directional information interaction; Secondly, analyzed the hardware system constraints caused by development of portable, mini-type GCS, as well as influences on GCS software design. Also, GCS software compatibility and interoperability standards and requirements were discussed. In the process of software design, at first, made a comprehensive analysis of the content of UAV data & information; Then finished the virtual instrument application design, put forward a multi-layer architecture model of 2D flight situation. The structure model analysis, data & information analysis provides a good guidance to the procedure of GCS software design & development, so as to avoid blindness and improve development efficiency. Virtual instrument interface design reflects the basic method of GUI (Graphical User Interface) design. The proposed multi-layer structure model of 2D flight situation shows the general scheme to solve the problem of navigation information output.
software architecture limitation factor user interface flight situation
Yiqi Kang Mei Yuan
School of Automation Science and Electrical Engineering,Beijing University of Aeronautics & Astronautics Beijing 100191,P.R.China
国际会议
2009 9th International Conference on Electronic Measurement & Instruments(第九届电子测量与仪器国际会议 ICEMI2009)
北京
英文
3965-3968
2009-08-16（万方平台首次上网日期，不代表论文的发表时间）