基于改进L1自适应控制方法的尾坐式垂直起降无人机过渡过程研究

Fanliang Meng, Congwei Zhao, Qianzhang Ren, Xinhua Wang
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引用次数: 0

摘要

尾倾式垂直起降无人机是一种新型的无人机,由于其在过渡过程中状态变化大、控制难度高,一直是国内外学者关注的焦点和难点。针对尾倾式垂直起降无人机在过渡过程中气动参数变化较大的问题,提出了一种改进的L1自适应控制方法。最后详细介绍了改进L1自适应控制器的设计过程,并进行了数字仿真,验证了改进L1自适应控制器在无人机过渡过程中的可行性和有效性。最后,给出了尾倾式垂直起降无人机整个过程的数字仿真结果并进行了分析。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Research of Tail-Sitter VTOL UAV in Transition Process Based on an Improved L1 Adaptive Control Method
The Tail-Sitter VTOL UAV is a new type of unmanned aerial vehicle (UAVS), and it has been the focus and difficulty of domestic and foreign scholars because of the large state changes and high control difficulty in the transition process. In this paper, an improved L1 adaptive control method was proposed to solve the problem that the aerodynamic parameters of Tail-Sitter VTOL UAV changed greatly during the transition process. Finally, the design process of the improved L1 adaptive controller is introduced in detail, and the digital simulation is carried out to verify the feasibility and effectiveness of the improved L1 adaptive controller in the UAV transition process. Finally, the digital simulation results of the whole process of Tail-Sitter VTOL UAV are given and analyzed.
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