Optimization Plug Mode of External Fuel and Weapons for Less Changing Aircraft Center of Gravity

Zhou Zeyang; Huang Jun; Yi Mingxu; Zhong Guo

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Optimization Plug Mode of External Fuel and Weapons for Less Changing Aircraft Center of Gravity

机译：飞机重心变化较小的外部燃料和武器的优化塞模式

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To achieve the minimum change of aircraft center of gravity, plugmode optimization was carried out. Plug mode, including weight and position of external fuel and weapon load, was selected as design mode. Numerical model for calculating aircraft center of gravity was established and used to generate mode samples. Random search algorithm (RSA) was designed and applied for solving the optimization plug mode, and the precise solution of plug mode was determined by full array method (FAM). Compared with typical plug mode, the optimization mode can reach a minimum change in aircraft center of gravity with fewer samples than the solution by FAM. RSA coupled with FAM is an effective scheme for the optimization of aircraft plug mode.

机译：为了实现飞机重心的最小变化，进行了塞模优化。选择包括外部燃料的重量和位置以及武器负载的插入模式作为设计模式。建立了计算飞机重心的数值模型，并将其用于生成模式样本。设计了随机搜索算法（RSA），并将其应用于优化插拔模式，并通过全阵列法（FAM）确定了插拔模式的精确解。与典型的插入模式相比，优化模式可以以比FAM解决方案更少的样本达到飞机重心的最小变化。结合FAM的RSA是优化飞机插头模式的有效方案。

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来源
《Mathematical Problems in Engineering》 |2017年第6期|1409829.1-1409829.8|共8页
作者
Zhou Zeyang; Huang Jun; Yi Mingxu; Zhong Guo;
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Beijing Univ Aeronaut & Astronaut, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China;

Beijing Univ Aeronaut & Astronaut, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China;

Beijing Univ Aeronaut & Astronaut, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China;

Beijing Univ Aeronaut & Astronaut, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China;

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1. Robust optimization of aircraft weapon delivery trajectory using probability collectives and meta-modeling [J] . Wang Nan, Shen Lincheng, Liu Hongfu, 中国航空学报（英文版） . 2013,第002期

机译：使用概率集合和元模型对飞机武器交付轨迹进行稳健的优化
2. Adaptive nonsingular fast terminal sliding mode control for aircraft with center of gravity variations [J] . Chan Han, Lingyu Yang, Jing Zhang Proceedings of the Institution of Mechanical Engineers . 2015,第g1期

机译：具有重心变化的飞机的自适应非奇异快速终端滑模控制
3. Development of equivalent model of external fuel tank assembly for dynamic characteristics analysis of aircraft [J] . Kim Hyun-Gi, Kim Sung Chan Aerospace science and technology . 2021,第Apra期

机译：用于飞机动态特性分析的外部燃料箱组件等效模型的开发
4. Study on change of aircraft center of gravity during fuel consumption [C] . Miao Yang, Wang Shaoping, Zhao Yongping IEEE 10th International Conference on Industrial Informatics . 2012

机译：飞机油耗过程中飞机重心变化的研究
5. Center-of-Gravity Estimation of an Aircraft Solely Using Traditional Aircraft Measurement Sensors. [D] . Komendat, Andrew J. 2012

机译：仅使用传统飞机测量传感器的飞机重心估计。
6. HS-SA-Based Precise Modeling of the Aircraft Fuel Center of Gravity Using Sensors Data [O] . Xiaoming Guo, Jing Zhang, Lin Tie, 2019

机译：使用传感器数据的基于HS-SA的飞机燃油重心精确建模
7. Optimization Plug Mode of External Fuel and Weapons for Less Changing Aircraft Center of Gravity [O] . Zeyang Zhou, Jun Huang, Mingxu Yi, 2017

机译：优化插头模式外部燃料和武器较不变的飞机重心

Optimization Plug Mode of External Fuel and Weapons for Less Changing Aircraft Center of Gravity

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