[1]雍 和,傅春啸,屈天祥,等.基于混合优化算法的直升机旋翼转速优化控制[J].机械与电子,2022,(05):66-71.
　YONG He,FU Chunxiao,QU Tianxiang,et al.Helicopter Rotor Speed Optimization Control Based on Hybrid Optimization Algorithm[J].Machinery & Electronics,2022,(05):66-71.
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基于混合优化算法的直升机旋翼转速优化控制()
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机械与电子[ISSN:1001-2257/CN:52-1052/TH]

卷:
期数:
2022年05期
页码:
66-71
栏目:
自动控制与检测
出版日期:
2022-05-24

文章信息/Info

Title:
Helicopter Rotor Speed Optimization Control Based on Hybrid Optimization Algorithm
文章编号:
1001-2257 ( 2022 ) 05-0066-06
作者:
雍 和; 傅春啸; 屈天祥; 滕 飞; 盛守照
南京航空航天大学自动化学院,江苏 南京 210016
Author(s):
YONG He ;  FU Chunxiao ;  QU Tianxiang ;  TENG Fei ;  SHENG Shouzhao
( College of Automation Engineering , Nanjing University of Aeronautics and Astronautics , Nanjing 210016 , China )
关键词:
变旋翼转速; 非线性优化; 遗传算法; 序列二次规划; 最小需用功率
Keywords:
variable rotor speed ;  nonlinear optimization ;  genetic algorithm ;  sequential quadratic programming ;  minimum power required
分类号:
V211 ; V249
文献标志码:
A
摘要:
为了实现直升机巡航飞行时最经济运行,基于某型常规布局直升机,建立巡航阶段需用功率目标函数,以飞行稳定性与操纵安全性指标作为约束条件,利用遗传 序列二次规划( GA-SQP )混合优化算法,对直升机巡航阶段实现最低需用功率的最优旋翼转速进行优化求解。实验结果表明,该方法得到的最优旋翼转速能够有效降低整机需用功率,优化算法得出的最优转速曲线对巡航状态下旋翼转速的变化方向具有一定参考意义。
Abstract:
In order to realize the most economical operation of helicopter in cruise flight , based on a certain type of conventional layout helicopter , a rotor required power objective function in cruise phase is established.Taking flight stability and handling safety indexes as constraints , the optimal rotor speed to achieve the minimum required power in helicopter cruise phase is solved by using GA-SQP hybrid optimization algorithm.The experimental results show that the optimal rotor speed obtained by this method can effectively reduce the required power of the whole helicopter , and the optimal speed curve obtained by the optimization algorithm has a certain reference significance for the change direction of rotor speed under cruise state.

参考文献/References:

[ 1 ] GUO W , HORN J.Rotor state feedback control for rotorcraft with variable rotor speed [ C ]// AIAA Guidance , Navigation , and Control Conference , 2009 : 5797.

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[ 5 ] 韩东 . 变转速旋翼直升机性能及配平研究[ J ] . 航空学报,2013 , 34 ( 6 ): 1241-1248.
[ 6 ] WAGNER R C.Procedural guide for modeling and analyzing the flight dynamics of the SH-60B helicopter using Flightlab [ R ] .California : Naval Postgraduate School Montery , 1995.
[ 7 ] 赵浩彬 . 基于改进遗传算法的 3D 打印多目标优化任务调度[ D ] . 天津:天津工业大学,2021.
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备注/Memo

备注/Memo:
收稿日期: 2021-10-21
作者简介:雍 和 ( 1997- ),男,江苏淮安人,硕士研究生,研究方向为飞行制导与控制;傅春啸 ( 1997- ),男,浙江绍兴人,硕士研究生,研究方向为先进飞行器控制;屈天祥 ( 1996- ),男,河南洛阳人,硕士研究生,研究方向为先进飞行器控制;滕 飞 ( 1997- ),男,江苏扬州人,硕士研究生,研究方向为导航制导与控制;盛守照 ( 1977- ),男,江苏南京人,教授,博士研究生导师,研究方向为无人飞行器先进控制技术。
更新日期/Last Update: 2022-05-26