| 1. | The application of adaptive control in aircraft landing gear is an important innovation to modern airplane design
自适应控制在飞机起落架的应用是一个比较新的课题。 |
| 2. | The research and discussion presented in this paper are semi - active control technology applied on the aircraft landing gear
本文对半主动控制技术在起落架上的应用做了研究和探讨。 |
| 3. | There are three control methods of aircraft landing gear : passive control , active control and semi - active control
对起落架的控制方法经历了被动控制、主动控制和较新的半主动控制三个过程。 |
| 4. | Meantime , according to the control model of aircraft landing gear , the adaptive control landing gear module was simulated through matlab
同时,根据起落架的控制模型,通过matlab仿真软件对采用自适应控制的起落架模型进行了仿真分析。 |
| 5. | Based on the stability and robustness of landing gear system , the adaptive control method was applied to the aircraft landing gear and the control model was acquired
基于起落架系统的稳定性和鲁棒性,采用自适应的控制方法对起落架系统进行设计,得到了起落架的控制模型。 |
| 6. | In order to possess high reliability , stability and long fatigue life during the landing and taxiing of aircraft , the design of aircraft landing gear is very important
如何使飞机在着陆和滑跑过程中具有较低的疲劳载荷、较好的稳定性、舒适性和较高的可靠性,起落架的设计至关重要。 |
| 7. | The development of semi - active control technology and the equipment : magnetorhelogical fluids damps based in this technology were introduced . the discussion presented in this paper is this equipment applied on the aircraft landing gear
本文分析了半主动控制技术的发展概况并构建了磁流变阻尼器,并对其在飞机起落架上的应用作了进行了初步探讨。 |
| 8. | Simulation results shows that adaptive control algorithm can make the output of aircraft landing gear approach to the reference output rapidly and the control system possess of good performance of robustness . hence , the control method is effective
仿真结果表明:自适应控制算法能够使起落架的控制变量快速达到理想的参考模型输出并且控制曲线平滑,同时控制系统具有很好的鲁棒性能,增强了系统的抗干扰能力。 |
| 9. | The paper mainly discussed and analyzed aircraft landing gear using model reference adaptive control and mcs ( minimal control synthesis algorithm ) , built up the mathematics model and linear state equations of aircraft landing gear during the landing and taxiing and analyzed the virtues of model reference adaptive and minimal control synthesis algorithm
本论文主要是采用模型参考自适应和最小控制综合算法( minimalcontrolsynthesisalgorithm )来描述飞机起落架系统,建立了完整的起落架着陆滑跑的数学模型和线性状态控制方程,分析了模型参考自适应和最小控制综合算法的优点。 |
| 10. | The control of aircraft landing gear is very complicated and the related research has barely begun although mcs algorithm can greatly improve the performance of aircraft landing gear if it was applied to landing gear . the author expects this paper can contribute to the design of aircraft landing gear
起落架的控制是复杂的控制,把最小控制综合算法应用于起落架的系统控制,将会使起落架的性能得到很大改善,但目前这方面的工作才刚刚开始,希望本文能对飞机起落架的设计提供一些参考和帮助。 |
