Low Thrust to Weight Ratio Manoeuvre of a Bio-inspired Bi-mode UAV
This paper explores the potential of a new aggressive rotational manoeuvre of a fixed-wing aircraft that has a turn radius less than its semi-span. A conceptual overview for a bi-mode bio-inspired UAV is given with particular focus given to the preliminary qualitative and quantitative analysis of rotational flight with low thrust to weight for hover and asymmetrical thrust to achieve enhanced rotational capability.
VTOL UAV rotary hover blade element turn radius manoeuvre
Derrick Ho Dr KC Wong1
School of Aerospace, Mechanical and Mechatronic Engineering, The University of Sydney
国际会议
2011年亚太航空航天技术学术会议(APISAT 2011)
澳大利亚
英文
1-9
2011-02-28（万方平台首次上网日期，不代表论文的发表时间）