论文:2013,Vol:31,Issue(2):223-228
引用本文:
王海涛, 蒋经凯. 飞机起落架主动控制与滑跑性能优化研究[J]. 西北工业大学
Wang Haitao, Jiang Jingkai. Active Control of Landing Gear and Taxiing Performance Optimization[J]. Northwestern polytechnical university

飞机起落架主动控制与滑跑性能优化研究
王海涛, 蒋经凯
西北工业大学 航空学院, 陕西 西安 710072
摘要:
起落架是飞机起飞、着陆、滑跑和地面停放的重要装置。为了提高飞机通过恶劣跑道的滑跑性能,研究了对起落架应用主动控制技术来实现飞机滑跑性能的优化。首先,将飞机视为刚体,建立了经典的二质量块模型。然后,应用最优控制理论和粒子群优化算法在Simulink环境下搭建模型和进行多目标优化计算,寻找广义PID(Proportional Integral Derivative)参数值。最后,通过计算机仿真研究了飞机通过弹伤修复跑道的响应,得出结论。基于粒子群算法的多目标最优PID控制是一种有效的控制方法,它可有效降低机身的受载,显著地改善飞机的地面滑跑性能。
关键词:    主动控制起落架    粒子群算法    最优控制    多目标最优    PID控制    仿真计算   
Active Control of Landing Gear and Taxiing Performance Optimization
Wang Haitao, Jiang Jingkai
College of Aeronautics,Northwestern Polytechnical University,Xi'an 710072,China
Abstract:
The landing gear is an important device that can enable airplane to take off,land,run and park. In or-der to improve the running performance of airplane which can run through bad runway,this paper studied the land-ing gear application of active control technology to achieving the optimization of the performance of airplane run-ning. First of all, we assumed the airplane to be a rigid body and established the classic two mass model. Then, weapplied optimal control theory and particle swarm optimization algorithm to build model and do multiobjective opti-mization calculations to search for generalized PID(Proportional Integral Derivative) parameter value in Simulinkenvironment. Finally,we drew a conclusion through computer simulation of the response of airplane runningthrough the runway that had been bombed and repaired. The multi-objective optimal PID control based on particleswarm optimization algorithm is an effective control method; it can effectively reduce the load and significantly im-prove the performance of running.
Key words:    aircraft    algorithms    calculations    computer simulation    control    landing gear(aircraft)    mathematicalmodels    multiobjective optimization    particle swarm optimization(PSO);active control of landing gear    optimal control    PID(Proportional Integral Derivative)control   
收稿日期: 2012-04-15     修回日期:
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作者简介: 王海涛(1972-),西北工业大学副教授、博士,主要从事飞行器设计、适航技术与研究及载运工具运用工程的研究。
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