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可垂直起降、高速前飞的飞行器设计与控制
引用本文:樊鹏辉,王新华,蔡开元.可垂直起降、高速前飞的飞行器设计与控制[J].控制理论与应用,2010,27(9):1171-1177.
作者姓名:樊鹏辉  王新华  蔡开元
作者单位:北京航空航天大学控制一体化技术重点实验室,北京,100191
基金项目:国家自然科学基金资助项目(60774008).
摘    要:本文设计了一种具有垂直起降、悬停和高速前飞能力的飞行器.这种飞行器通过模态转换,既能够实现类似传统四轴飞行器的垂直起降,又能够实现类似固定翼飞行器的高速前飞.同时本文针对这种飞行器设计了模态转换控制律;仿真试验验证了设计方案和控制律的有效性.

关 键 词:垂直起降    高速前飞    模态转换    四轴飞行器    固定翼
收稿时间:2009/4/16 0:00:00
修稿时间:2009/10/13 0:00:00

Design and control of aircraft of vertical take-off-and-landing and high-speed forward flight
FAN Peng-hui,WANG Xin-hua and CAI Kai-yuan.Design and control of aircraft of vertical take-off-and-landing and high-speed forward flight[J].Control Theory & Applications,2010,27(9):1171-1177.
Authors:FAN Peng-hui  WANG Xin-hua and CAI Kai-yuan
Affiliation:National Key Laboratory of Science and Technology on Holistic Control, Beihang University,National Key Laboratory of Science and Technology on Holistic Control, Beihang University,National Key Laboratory of Science and Technology on Holistic Control, Beihang University
Abstract:We design a new aircraft with the ability of vertical take-off-and-landing(VTOL), like a four-rotor aircraft; and the ability of flying forward with high speed, like an aircraft with fixed-wings. The flight-mode transition from hovering to forward flight and the reverse process are achieved. A flight-mode transition control law is designed. Both the designscheme and the proposed control law are verified by simulation.
Keywords:VTOL  high-speed forward flight  flight-mode transition  four-rotor aircraft  fixed-wings
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