Flight Simulation Testbed of Unmanned Helicopter

摘要：

This paper designed a flight simulation testbed of unmanned helicopter. This testbed has the advantage of simple structure, easy implement, low cost, convenient movement and so on. It is suitable for various flight test of mini-unmanned helicopter. It provides attitude needed by unmanned helicopter, such as pitch, yaw, roll and so on, to ensure that unmanned helicopter can be free flight within a certain range. Making use of the testbed can reproduce the actual flight of unmanned helicopter under laboratory conditions, and can be very convenient for attitude control, flight control, navigation and other scientific researches; accordingly, it ensures the security of flight test for unmanned helicopter.

关键词： unmanned helicopter flight simulation testbed

作者: Jiande Wu Ting Feng Yugang Fan

作者单位: Faculty of Information Engineering and Automation Kunming University of Science and Technology Kunming, CHINA

会议类型: 国际会议

会议名称: Second International Symposium on Information Science and Engineering(第二届信息科学与工程国际会议)

会议地点: 上海

会议语种:英文

页码: 497-499

在线出版日期: 2009-12-26（万方平台首次上网日期，不代表论文的发表时间）