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2024 Aerospace & Electronic Systems Society: Organization and Representatives 2024 航空航天与电子系统学会:组织和代表
IF 3.6 3区 工程技术 Q1 ENGINEERING, AEROSPACE Pub Date : 2024-07-09 DOI: 10.1109/maes.2024.3417800
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引用次数: 0
IEEE Aerospace and Electronic Systems Magazine Publication Information 电气和电子工程师学会《航空航天与电子系统》杂志出版信息
IF 3.6 3区 工程技术 Q1 ENGINEERING, AEROSPACE Pub Date : 2024-07-09 DOI: 10.1109/maes.2024.3417796
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引用次数: 0
AESS Awards Deadline AESS 奖项截止日期
IF 3.6 3区 工程技术 Q1 ENGINEERING, AEROSPACE Pub Date : 2024-07-09 DOI: 10.1109/maes.2024.3417871
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引用次数: 0
Share Your Preprint Research with the World! 与世界分享您的预印本研究成果
IF 3.6 3区 工程技术 Q1 ENGINEERING, AEROSPACE Pub Date : 2024-07-09 DOI: 10.1109/maes.2024.3417877
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引用次数: 0
In This Issue –Technically 本期内容 - 技术
IF 3.6 3区 工程技术 Q1 ENGINEERING, AEROSPACE Pub Date : 2024-07-09 DOI: 10.1109/maes.2024.3417857
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引用次数: 0
IEEE Autotestcon 2024 电气和电子工程师学会 Autotestcon 2024 年会议
IF 3.6 3区 工程技术 Q1 ENGINEERING, AEROSPACE Pub Date : 2024-07-09 DOI: 10.1109/maes.2024.3417869
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引用次数: 0
From the Editor-in-Chief 主编的话
IF 3.6 3区 工程技术 Q1 ENGINEERING, AEROSPACE Pub Date : 2024-07-09 DOI: 10.1109/maes.2024.3415234
Pau Closas
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引用次数: 0
A Heterogeneous, Autonomous Passive Network for Underwater Surveillance. Experimental Results with Real Data Collected at Sea 用于水下监视的异构自主无源网络。利用海上采集的真实数据得出的实验结果
IF 3.6 3区 工程技术 Q1 ENGINEERING, AEROSPACE Pub Date : 2024-07-04 DOI: 10.1109/maes.2024.3421408
Alessandra Tesei, Pietro Stinco, Gabriele Ferri, Murat Uney, Robert Been, Kevin D. LePage
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引用次数: 0
Optimized Digital Simulation Methodology for System Validation Using Real-Time Hardware-in-Loop Simulation Platform 利用实时硬件在环仿真平台进行系统验证的优化数字仿真方法学
IF 3.6 3区 工程技术 Q1 ENGINEERING, AEROSPACE Pub Date : 2024-06-11 DOI: 10.1109/maes.2024.3412034
Rajesh S. Karvande, Madhavi Tatineni
Validation of onboard software is an essential and mandatory step before real launch in the aerospace and defense industry. This validation platform is popularly known as hardware-in-loop (HIL) simulation. It evaluates the real-time performance of the embedded system software and this is the tool to resolve the problems related to design, subsystem integration, and real-time execution by creating a modeling and simulation plant simulation platform. There are different configurations of HILS to validate every avionics subsystem like onboard computers, actuators, sensors, etc. In this article, development of an HIL simulation setup for a newly adopted fully digital controller for avionics configuration is discussed. This article looks at the development of a new configuration that is based on a fully digital feedback signal at a faster rate as required by the plant model so that the subsystem can be tested efficiently without causing any undue delay and oscillation in HIL methodology. The general methodology to test the actuator is to send a command to this system and take position feedback to the plant model with continuous analog signal for faster execution of the 6Dof algorithm. However, in the newly developed method discussed in this article; the plant model is configured using discrete digital signals instead of continuous signal feedback from the subsystem. The system approach for validation of this system, different methodologies as well as the synchronization and elimination of delay in simulation computer is elaborated.
在航空航天和国防工业中,机载软件的验证是真正发射前必不可少的强制步骤。这种验证平台俗称 "硬件在环 (HIL) 仿真"。它评估嵌入式系统软件的实时性能,是通过创建建模和仿真工厂仿真平台来解决与设计、子系统集成和实时执行相关问题的工具。HILS 有不同的配置,可用于验证机载计算机、执行器、传感器等每个航空电子子系统。本文将讨论为航空电子配置新采用的全数字控制器开发 HIL 仿真设置。本文探讨了基于全数字反馈信号的新配置的开发过程,该配置可按照工厂模型的要求以更快的速度进行测试,从而在 HIL 方法中有效地测试子系统,而不会造成任何不必要的延迟和振荡。测试执行器的一般方法是向该系统发送指令,并通过连续模拟信号向工厂模型提供位置反馈,以便更快地执行 6Dof 算法。然而,在本文讨论的新开发方法中,工厂模型是使用离散数字信号配置的,而不是来自子系统的连续信号反馈。本文阐述了验证该系统的系统方法、不同的方法以及模拟计算机的同步和消除延迟。
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引用次数: 0
Radar Altimeter Coexist Design in the 4.2-4.4 GHz Band for Multi-Stage Interference Risk Mitigation in 5G and Beyond 在 4.2-4.4 千兆赫频段上进行雷达高度计共存设计,以降低 5G 及其他技术的多级干扰风险
IF 3.6 3区 工程技术 Q1 ENGINEERING, AEROSPACE Pub Date : 2024-06-11 DOI: 10.1109/maes.2024.3412858
Jarret Rock, Ying Wang
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引用次数: 0
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