攻击角和侧滑角的估计以及民用飞机的补充波器设计
Shaobo Zhai1, Guangwen Li1, Penghui Huang2
1School of Automation, Northwestern Polytechnical University, Xi'an 710072, China.
ISA transactions
|August 23, 2024
概括
这项研究通过改善飞机的攻击角 (AOA) 和侧滑角 (AOS) 估计来提高飞行安全. 新的方法增加了冗余性和准确性,确保可靠的机载系统性能.
科学领域:
- 航空航天工程 航空航天工程
- 飞行动力学和控制控制
背景情况:
- 准确的攻击角度 (AOA) 和侧滑角度 (AOS) 对飞行安全和机载系统性能至关重要.
- 现有的方法可能缺乏关键飞行参数的足够冗余性和准确性.
研究的目的:
- 开发民用飞机中AOA和AOS的增强估计方法.
- 为了提高空气流角度测量的冗余性和准确性.
- 为更可靠的飞行数据设计补充过器.
主要方法:
- 为冗余的AOA和AOS估计,开发了一种具有加速度校正的扩展卡尔曼波器.
- 引入了一种新的惯性计算方法,用于AOA和AOS,使用态度,近向和飞行路径角度.
- 为了提高准确性,展示了使用图斯变换的两个离散互补过器设计.
主要成果:
- 开发的算法成功估计了AOA和AOS,并提高了冗余性和准确性.
- AOA估计误差在±0.6度之内.
- AOS估计误差在±0.3度之内.
结论:
- 提出的方法有效地提高了AOA和AOS估计的准确性和冗余性.
- 开发的算法提供了可靠的空气流角度数据,这对于飞行安全和系统运行至关重要.
- 该研究验证了扩展卡尔曼波器和补充波器设计用于飞机飞行参数估计的有效性.
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