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| 新型歼击机空中加油飞行仿真建模研究 | |
| 引用本文： | 隋成城,由勇,杨永田,由俊生.新型歼击机空中加油飞行仿真建模研究[J].系统仿真学报,2005,17(6):1336-1338. |
| 作者姓名： | 隋成城 由勇 杨永田 由俊生 |
| 作者单位： | 1. 哈尔滨工程大学计算机科学与技术学院,哈尔滨,150001 2. 清华大学自动化系,北京,100084 3. 空军第四研究所,北京,100036 |
| 摘 要： | 空中加油是提高飞机作战能力的重要手段。空中加油模拟训练成了培养飞行员空中加油技术的重要途径。空中加油飞行的数学建模是模拟加油飞行的理论基础，它直接关系到模拟飞行的逼真程度，关系到模拟加油训练的效果。研究了大型授油机尾流的形成和分布特点，分析了受油机在不同位置进入黾流时飞机所受的影响，提出了相应的数学建模方法。同时分析了新型歼击机在加油过程中飞机质量和重心的变化规律和对飞行性能的影响。 |
| 关 键 词： | 空中加油 飞行仿真 建模 尾流 |
| 文章编号： | 1004-731X(2005)06-1336-03 |
| 修稿时间： | 2004年7月24日 |
Modeling and Simulation of In-flight Fueling for a New Type of Fighter |
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| SUI Cheng-cheng,YOU Yong,YANG Yong-tian,YOU Jun-sheng.Modeling and Simulation of In-flight Fueling for a New Type of Fighter[J].Journal of System Simulation,2005,17(6):1336-1338. | |
| Authors: | SUI Cheng-cheng YOU Yong YANG Yong-tian YOU Jun-sheng |
| Institution: | SUI Cheng-cheng1,YOU Yong2,YANG Yong-tian1,YOU Jun-sheng3 |
| Abstract: | In-flight fueling of fighter is one of the most important methods to improve the battle effectiveness of Air Force. Real-time modeling of in-flight fueling is the key part of in-flight fueling simulation system. The formation and distribution of wake flow behind a large aerial tanker are discussed, Then the mathematic model of disturbance to the refueled aircraft during refueling is given. And, the change of total mass and CG of refueled aircraft during refueling will cause the change of stability and controllability. |
| Keywords: | in-flight fueling flight simulation modeling wake |
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