一种基于仿真预测的编队射频兼容试飞方法

孙利娜 ,  陈宇 ,  汪真

科学技术与工程 ›› 2025, Vol. 25 ›› Issue (14) :6094-6099

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科学技术与工程 ›› 2025, Vol. 25 ›› Issue (14) :6094-6099 DOI: 10.12404/j.issn.1671-1815.2404270
航空、航天

一种基于仿真预测的编队射频兼容试飞方法

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A Flight Test Method for Formation RF Systems Compatibility Based on Simulation Prediction

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摘要

编队射频兼容是影响编队生存力和战斗力的一项重要综合能力,需通过飞行试验对其进行有效考核验证,仿真预测可进一步优化试验设计,提升试验效费比。基于此,提出了一种基于仿真预测的编队射频兼容试飞方法。首先分析了射频兼容的发展趋势和编队射频兼容能力要求,其次提出了基于干扰冲突的编队射频兼容仿真预测模型,并以仿真分析的干扰冲突距离为依据,建立了编队射频兼容试飞剖面设计方法。最后,进行了典型编队射频兼容试飞试验的仿真分析和试飞剖面设计。研究结果为编队射频兼容的试验剖面设计和试飞验证提供了一种有效方法。

Abstract

Formation RF (radio frequency) systems compatibility is an important comprehensive ability that affects the survival and combat effectiveness of aircraft formation. It needs to be effectively assessed and verified through flight tests, and simulation can further optimize test design and improve test efficiency. Thus, a flight test method for formation RF systems compatibility based on simulation prediction was proposed. Firstly, the development trend of RF compatibility and is its capability requirements were summarized and analyzed. Secondly, a simulation model of formation RF systems compatibility based on interference conflict was proposed, and a flight test method of formation RF systems compatibility based on the interference conflict distance from simulation analysis was established. Finally, simulation analysis and flight profile design were conducted for a typical formation RF compatibility test. This study has provided an effective method for the test profile design and flight verification of formation RF systems compatibility.

关键词

编队射频兼容 / 干扰冲突模型 / 飞行试验 / 试验剖面设计

Key words

formation RF systems compatibility / interference conflict model / flight test / test profile design

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孙利娜, 陈宇, 汪真. 一种基于仿真预测的编队射频兼容试飞方法[J]. 科学技术与工程, 2025, 25(14): 6094-6099 DOI:10.12404/j.issn.1671-1815.2404270
SUN Li-na, CHEN Yu, WANG Zhen. A Flight Test Method for Formation RF Systems Compatibility Based on Simulation Prediction[J]. Science Technology and Engineering, 2025, 25(14): 6094-6099 DOI:10.12404/j.issn.1671-1815.2404270

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