The Design and Performance Analysis of Hybrid Dynamical System with Multil-Rotor UAV
Abstract: According to multi-rotor unmanned aerial vehicle’s disadvantages and the structure characteristic at the present, a hybrid dynamical system is being put forward for solving this relevant issue. Have designed and calculated with the hybrid dynamical system for multi-rotor unmanned aerial vehicle, and used the MATLAB/Simulink software to establish the hybrid dynamical system simulation model, there are some simulation and performance analysis for the hybrid dynamical system’s design. The results show that the hybrid dynamical system has the lower fuel consumption characteristic than single two-cycle engine in the same condition that type and output power and the hybrid dynamical system have the high reliability and without artificial recharge advantages, it also can reduce the multi-rotor unmanned aerial vehicle depending on battery when it needs to fly longer and reduce the demand with two-cycle engine’s reliability.
文章引用: 宗 剑 , 王 云 , 毛鞠盛 (2016) 多旋翼UAV混合动力系统设计与性能分析。 国际航空航天科学， 4， 25-33. doi: 10.12677/JAST.2016.42004
 杨益军. 植保无人机飞入千亿市场蓝海可期[J]. 中国农药, 2015(12): 48-55.
Hung, J.Y. and Gonzalez, L.F. (2012) On Parallal Hybrid-Electic Propusion System for Unmanned Aerial Verial Vehicles. Progress in Aerospace Science, 51, 1-17.
 周宝龙, 刘忠长, 高宗英. 内燃机学[M]. 北京: 机械工业出版社, 2010: 67-72.
 吴影生. 永磁无刷直流电机起动/发电系统研究[M]. 南京: 东南大学, 2004: 17-25.
 陈根, 程启明, 李明, 等.电动汽车中锂电池两种建模方式的分析与比较[J]. 电源技术, 2014(11): 2051-2054.