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Updated: Jun 21, 2025

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动力学建模和非线性态度控制器设计用于火箭型无人驾驶飞行器
Chao-Hsien Chih1, Yang-Rui Li1, Chao-Chung Peng1
1Department of Aeronautics and Astronautics, National Cheng Kung University, Tainan, 701, Taiwan.
ISA transactions
|July 16, 2024
概括
这项研究引入了一种新的火箭型无人机 (UAV),具有推力向量控制 (TVC),使用基于杆的同轴转子系统 (GCRS). 一个PID和Levenberg-Marquardt算法有效地管理复杂的控制分布,以实现稳定的飞行.
科学领域:
- 航空航天工程 航空航天工程
- 控制系统 控制系统
- 机器人技术 机器人技术 机器人技术
背景情况:
- 火箭型无人机 (UAV) 需要复杂的控制系统来稳定飞行.
- 基于杆的同轴转子系统 (GCRS) 提供推力向量控制 (TVC),但存在复杂的非线性控制分布挑战.
研究的目的:
- 开发和验证用于用于TVC的GCRS的新型火箭型无人机的高度和态度控制系统.
- 为了解决GCRS执行中固有的高度非线性和紧密合的控制分配问题.
主要方法:
- 导出无人机的态度飞行动态.
- 开发一种使用线性矩阵不等式 (LMI) 实现强大的稳定性的比例整数导数 (PID) 控制算法.
- 应用Levenberg-Marquardt (LM) 优化方法来解决非线性控制输入分布问题.
主要成果:
- 成功实施控制策略,以追踪所需的态度轨迹.
- 对GCRS执行器输出的非线性反向映射问题的有效解决方案.
- 经过证明的态度稳定和高度跟踪能力,即使在干扰下.
结论:
- 拟议的基于GCRS的TVC系统是火箭型无人机的可行方法.
- 联合PID和LM控制算法有效地解决了复杂的控制分配挑战.
- 数字模拟证实了系统能够实现强大的态度和高度控制的能力.
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