Semi-Autonomous Aerobatics of Fixed-Wing UAV

被引:0
|
作者
Min, Sun-Ki [1 ]
Park, Sanghyuk [1 ]
机构
[1] Korea Aerosp Univ, Goyang Si, South Korea
关键词
Semi-Autonomous; Aerobatics; Specific Force Acceleration; Control Law;
D O I
10.5139/JKSAS.2024.52.9.689
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In this study, control laws for unskilled pilots to easily perform aerobatic maneuvers and a control mode that allows for a seamless transition between normal and aerobatic flight with simple pilot inputs are proposed. The aerobatic control laws are based on the specific force acceleration control loops and the introduction of z-axis reference vector. The designed control system and control mode are implemented using a low-cost platform, and their control performance and handling quality are validated through MATLAB Simulink-based simulations and actual flight tests.
引用
收藏
页码:689 / 697
页数:9
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