首页|基于改进舰尾流模型和多层耦合分析的机载雷达测量建模

基于改进舰尾流模型和多层耦合分析的机载雷达测量建模

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为提高复杂海洋环境中无人舰载机(Unmanned carrier-based aircraft,UCA)自动着舰时导航定位的准确性,研究舰尾流对机载雷达测量过程的动态影响问题,建立一种基于多层级耦合性分析的测量影响动态建模分析方法.首先,利用直接分解法和前向差分法建立一种基于离散化状态空间的时变舰尾流模型,以克服传统传递函数方法存在的局限性;其次,基于舰尾流各分量均与飞机飞行速度相关的客观事实,通过在时变系统中考虑舰尾流分量间的相互作用关系来构建一种更符合实际系统特征的分量自耦合舰尾流模型;紧接着,采用UCA姿态角变化能够改变坐标转换矩阵的思想,研究舰尾流与UCA位姿变化间的耦合联系,提出一种准确性更高的舰尾流对UCA位姿的深度影响模型;然后,以航母姿态变化对舰载雷达测量结果的影响模型为基础,通过考虑本研究场景的内在特性,建立UCA姿态变化对雷达测量结果的影响模型分析方法;紧接着,采用示意图方式获得位移变化对机载雷达测量结果的影响模型;最后,针对舰船受海洋大气(风、浪、流)干扰而出现失速这一现象,建立实际海洋环境中舰尾流对机载雷达测量结果的非线性非高斯影响分析模型.仿真实验研究验证了上述模型分析方法的有效性和优越性.
Airborne Radar Measurement Modeling Based on Improved Carrier Air Wake Model and Multi-layer Coupling Analysis
To improve the accuracy of navigation and positioning for unmanned carrier-based aircraft(UCA)auto-matic landing in complex marine environments,this study investigated the dynamic effects of carrier air wake on onboard radar measurements and established a modeling and analysis method based on multi-level coupling analys-is.Firstly,a time-varying carrier air wake model based on a state-space discretization approach using direct decom-position and forward differences was developed to overcome the limitations of traditional transfer function methods.Secondly,a component self-coupling carrier air wake model was constructed to be more consistent with actual sys-tem characteristics by considering the interaction between components,which are all related to the aircraft's flight speed.Thirdly,a more accurate depth effect model of carrier air wake on UCA's position was proposed by study-ing the coupling relationship between carrier air wake and UCA's attitude changes through the concept of coordin-ate transformation matrices.Subsequently,an analysis method of the effect of UCA's attitude changes on radar measurements was developed based on the impact of aircraft carrier attitude changes on radar measurements.Then,a displacement change effect model on onboard radar measurements was obtained using a diagrammatic approach.Finally,a nonlinear and non-Gaussian effect analysis model of carrier air wake on onboard radar measurements in actual marine environments was established to address aircraft stalling caused by atmospheric disturbances such as wind,waves,and currents.Simulation experiments showed the effectiveness and superiority of the proposed model-ing and analysis methods.

Carrier air wakeairborne radarstate spacecouplingnonlinear non-Gaussian

葛泉波、王远亮、李宏

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南京信息工程大学自动化学院 南京 210044

江苏省大气环境与装备技术协同创新中心 南京 210044

江苏省大数据分析技术重点实验室 南京 210044

上海海事大学物流工程学院 上海 200135

中国飞行试验研究院 西安 710089

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舰尾流 机载雷达 状态空间 耦合性 非线性非高斯

国家自然科学基金国家自然科学基金江苏省"青蓝工程"项目

62033010U23B2061R2023Q07

2024

自动化学报
中国自动化学会 中国科学院自动化研究所

自动化学报

CSTPCD北大核心
影响因子:1.762
ISSN:0254-4156
年,卷(期):2024.50(3)
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