固定翼
航空航天工程
飞行包线
飞机飞行力学
控制理论(社会学)
弹道
翼
推力
模式(计算机接口)
飞行管理系统
过渡(遗传学)
推进
电传电报
工程类
模拟
计算机科学
控制(管理)
飞行模拟器
空气动力学
物理
人工智能
基因
化学
操作系统
生物化学
天文
作者
Zihuan Cheng,Hailong Pei
出处
期刊:IEEE robotics and automation letters
日期:2022-01-25
卷期号:7 (2): 3106-3113
被引量:8
标识
DOI:10.1109/lra.2022.3145087
摘要
For agile fixed-wing aerial robots, the vertical/horizontal flight mode transition is a fundamental requirement for high maneuverability. This letter focuses on a challenging implementation in which the aircraft conducts the transitional flight at fixed altitude along a straight path. Implemented on a small ducted fan fixed-wing, we propose a transition-corridor-based control strategy to conduct the flight transition neatly. The transition corridor is described as a region comprising all the admissible flight velocities, accelerations and attitudes, bounded by the capacity of both the propulsion and control system of the vehicle. By planning the transition trajectory in obedience with the identified transition corridor, as well as adopting a unified full envelope flight control scheme, the ducted fan fixed-wing successfully accomplishes the practical transitional flight. Experimental results are satisfactory in both flight mode transition and altitude stabilization.
科研通智能强力驱动
Strongly Powered by AbleSci AI