TY - GEN
T1 - Software design for mini-type ground control station of UAV
AU - Kang, Yiqi
AU - Yuan, Mei
PY - 2009
Y1 - 2009
N2 - The guiding ideology and principle of GCS (Ground Control Station) software design & development were proposed by analyzing the role of CGS in UAV (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.
AB - The guiding ideology and principle of GCS (Ground Control Station) software design & development were proposed by analyzing the role of CGS in UAV (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.
KW - Flight situation
KW - Limitation factor
KW - Software architecture
KW - User interface
UR - https://www.scopus.com/pages/publications/71549117611
U2 - 10.1109/ICEMI.2009.5274691
DO - 10.1109/ICEMI.2009.5274691
M3 - 会议稿件
AN - SCOPUS:71549117611
SN - 9781424438624
T3 - ICEMI 2009 - Proceedings of 9th International Conference on Electronic Measurement and Instruments
SP - 4737
EP - 4740
BT - ICEMI 2009 - Proceedings of 9th International Conference on Electronic Measurement and Instruments
T2 - 9th International Conference on Electronic Measurement and Instruments, ICEMI 2009
Y2 - 16 August 2009 through 19 August 2009
ER -