Model-Based Design of UAV Autopilot Software

摘要：

　　This paper presents a Model-Based approach to develop UAV (Unmanned Aerial Vehicle) autopilot software.It employs Simulink to design the flight controller,Stateflow to implement control logic and Matlab coder to automatically generate embedded C code from the model developed.Software in the loop (SIL) and hardware in the loop (HIL) simulations are performed in the laboratory to validate the software developed.Flight trial cost and risks are minimized and the design cycles are greatly shortened.The feasibility and the effectiveness of the approach are verified through results from lab simulations and field trials.

关键词： UAV model-based design flight control simulation

作者: Zuo Ming Liu Ying Qian Yi Hu Xiongwen Zhao Xiaochuan Wang Jinhua

作者单位: Beijing Institute of Computer Application Beijing, China China academy of ordnance science Beijing, China

会议类型: 国际会议

会议名称: 2012 2nd International Conference on Computer and Information Applications(ICCIA2012)(2012第二届计算机和信息应用国际会议)

会议地点: 太原

会议语种:英文

页码: 1174-1178

在线出版日期: 2012-12-08（万方平台首次上网日期，不代表论文的发表时间）