Model System Design for Small-size Unmanned Helicopter Based on Moment Theory,Blade Element Theory and FlightLab Software

摘要：

Model system based on moment theory, blade element theory and FlightLab software is designed for small-size unmanned helicopter. The system includes three models of helicopter, moment theory model (MTM), blade element theory model (BETM) and FlightLab model (FLM). MTM is used mainly for performance analysis, BETM for control system design and FLM for nonlinear real-time simulation. Then a high-reliable model system is realized by analysis and compare. The model system has good effect by simulations and fly tests.

作者: Wang Xiaoqing Huang Yimin

作者单位: College of Automation Engineering,NanJing University of Aeronautics and Astronautics Nanjing,210016,China

会议类型: 国际会议

会议名称: The 2nd International Symposium on Systems and Control in Aeronautics and Astronautics(第二届航空航天系统与控制国际会议 ISSCAA 2008)

会议地点: 深圳

会议语种:英文

页码: 876-879

在线出版日期: 2008-12-10（万方平台首次上网日期，不代表论文的发表时间）