基于恒模惩罚准则的鲁棒自适应波束形成器

IF 1.1 4区 工程技术 Q3 ENGINEERING, AEROSPACE
Chuanhui Hao, Bin Zhang, Xubao Sun
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引用次数: 0

摘要

为了提高阵列波束形成的鲁棒性,本文提出了一种基于恒模准则的鲁棒自适应波束形成器,该波束形成器是一种重构最小优化方法,用于解决由导向矢量失配引起的权向量失配问题。在全球定位系统(GPS) L1频段,首先通过设计双极化天线阵列对GPS阵列信号进行建模。其次,分析了传统最小方差无失真响应波束形成系统中波束形成的失真问题。为了修复权向量失配问题,提出了一种基于CM包络响应的新型波束形成器,在阵列处理过程中重构MVDR波束形成。此外,在对MVDR波束形成器响应进行惩罚时,采用最小-最大惩罚准则使波束形成器能够分配更多的自由度。最后,设计了一个辅助的二元实变量来规划所提出的波束形成器。但它仍然是一个非凸二次规划问题,因此采用交替方向乘法器(ADMM)将目标函数转化为若干子问题。数值模拟结果验证了该波束形成器的有效性,并将其与现有的波束形成器进行了比较。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Robust Adaptive Beamformer Based on Constant Modulus Penalty Criteria
In this study, a robust adaptive beamformer based on constant modulus (CM) criteria is developed to improve the robustness of the array beamforming, which is a reconstructing minimal optimization for solving the mismatch problem of weight vector caused by steering vector mismatch. In the global positioning system (GPS) L1 band, firstly, a GPS array signal is modelled by designing a dual-polarized antenna array. Secondly, the distortion problem of beamforming is formulated in the traditional minimum variance distortionless response (MVDR) beamformer. For repairing the weight vector mismatch problem, a novel beamformer based on the CM envelope response is proposed to reconstruct MVDR beamforming in the array processing. Besides, min-max penalty criteria are used to enable the beamformer to allocate more degrees of freedom (DOFs) when penalizing the MVDR beamformer responses. Finally, an auxiliary two-element real variable is designed to plan the proposed beamformer. But it is still a nonconvex quadratic programming problem, so an alternating direction method of multipliers (ADMM) is employed to transform the objective function into several subproblems. Illustrative numerical simulation results are provided for validating the effectiveness of the proposed beamformer by comparing it with other existing approaches.
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来源期刊
CiteScore
2.70
自引率
7.10%
发文量
195
审稿时长
22 weeks
期刊介绍: International Journal of Aerospace Engineering aims to serve the international aerospace engineering community through dissemination of scientific knowledge on practical engineering and design methodologies pertaining to aircraft and space vehicles. Original unpublished manuscripts are solicited on all areas of aerospace engineering including but not limited to: -Mechanics of materials and structures- Aerodynamics and fluid mechanics- Dynamics and control- Aeroacoustics- Aeroelasticity- Propulsion and combustion- Avionics and systems- Flight simulation and mechanics- Unmanned air vehicles (UAVs). Review articles on any of the above topics are also welcome.
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