VTOL

作品数：69被引量：128H指数：7
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相关领域：航空宇航科学技术自动化与计算机技术更多>>
相关作者：邹立颖刘金琨苗凤娟袁瑞侠刘帅更多>>
相关机构：北京航空航天大学北方工业大学齐齐哈尔大学威罗门飞行公司更多>>
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相关基金：国家自然科学基金国家教育部博士点基金中国博士后科学基金中央级公益性科研院所基本科研业务费专项更多>>
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Fast level-flight to hover mode transition and altitude control in tiltrotor’s landing operation
《Chinese Journal of Aeronautics》2021年第1期181-193,共13页Ningjun LIU Zhihao CAI Yingxun WANG Jiang ZHAO 
co-supported by the Beijing Municipal Sci-Tech Program (No. Z181100003218015);the Fundamental Research Funds for the Central Universities, China (No. YWF-20-BJ-J-542)。
An attempt is made to implement a faster level-flight to hover mode transition in tiltrotor’s landing process for the purpose of shortening its landing time. A three-stage tiltrotor landing maneuver is designed, and ...
关键词：TILTROTOR Transition Flight control VTOL UAV ADRC 
Trajectory tracking control of a VTOL unmanned aerial vehicle using offset-free tracking MPC被引量：13
《Chinese Journal of Aeronautics》2020年第7期2024-2042,共19页Tayyab MANZOOR Yuanqing XIA Di-Hua ZHAI Dailiang MA 
co-supported by the National Natural Science Foundation of China(Nos.61225015,61105092,61422102,and 61703040);the Beijing Natural Science Foundation,China(No.4161001);the China Postdoctoral Science Foundation(No.2017M620640)。
Designing a stable and robust flight control system for an Unmanned Aerial Vehicle(UAV)is an arduous task.This paper addresses the trajectory tracking control problem of a Ducted Fan UAV(DFUAV)using offset-free Model ...
关键词：Autonomous flight control Model Predictive Control(MPC) Time delays Trajectory tracking Unmanned Aerial Vehicle(UAV) 
Predictor-based model reference adaptive roll and yaw control of a quad-tiltrotor UAV被引量：12
《Chinese Journal of Aeronautics》2020年第1期282-295,共14页Ningjun LIU Zhihao CAI Jiang ZHAO Yingxun WANG 
An attempt is made to apply modern control technology to the roll and yaw control of a rudderless quad-tiltrotor Unmanned Aerial Vehicle(UAV)in the latter part of the flight mode transition,where aerodynamic forces on...
关键词：Adaptive CONTROL Flight CONTROL TILTROTOR UAV VTOL 
Conceptual design and optimization of a tilt-rotor micro air vehicle被引量：7
《Chinese Journal of Aeronautics》2019年第2期369-381,共13页M.HASSANALIAN R.SALAZAR A.ABDELKEFI 
the financial support from New Mexico Space Grant Consortium
The conceptual design and optimization of a tilt-rotor Micro Air Vehicle(MAV) for a well-defined mission are performed. The objective of this design cycle is to decrease the design time in order to efficiently create ...
关键词：Aerodynamic analysis SIZING Tilt-rotor MAV VTOL STABILITY 
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