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681.
本文阐述了DSP(TMS320C240)的基本结构,指出该DSP计算速度快,具有PWM波形发生器等特点,并将DSP芯片应用于电机的矢量控制系统中,同时给出了控制系统的软件及硬件设计图。 相似文献
682.
电阻点焊质量控制系统的研究 总被引:1,自引:0,他引:1
分析了利用动态电极压力监控点焊质量的原理,利用压电石英力传感器、负荷放大器及其外围电路,建立了动态电极压点焊质量控制系统。介绍了控制系统硬件结构和控制软件设计。实验结果表明,采用该控制系统能够有效地控制焊点质量。 相似文献
683.
以某大型民用客机为例,基于各系统的功能危险性评估报告进行故障筛选,根据筛选得到的故障清单对失效发生时刻和失效状态下继续飞行的飞行载荷进行了设计分析,发展形成了一种高效、可靠的故障载荷设计研究方法。 相似文献
684.
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686.
介绍了一种基于AVR单片机的步进电机控制系统,快速实现步进电机的加速-匀速-减速-定位的运行控制,在实现精确定位运行的情况下还可以实现运行时间的控制,详细分析了其实现原理,并对定位误差进行了实际测量,改变了传统的开环位置控制方法,提升了定位控制精度。 相似文献
687.
《中国航空学报》2016,(1):76-90
Gust load alleviation (GLA) tests are widely conducted to study the effectiveness of the control laws and methods. The physical parameters of models in these tests are aeroelastic scaled, while the scaling of GLA control system is always unreached. This paper concentrates on studying the scaling laws of GLA control system. Through theoretical demonstration, the scaling criterion of a classical PID control system has been come up and a scaling methodology is provided and veri-fied. By adopting the scaling laws in this paper, gust response of the scaled model could be directly related to the full-scale aircraft theoretically under both open-loop and closed-loop conditions. Also, the influences of different scaling choices of an important non-dimensional parameter, the Froude number, have been studied in this paper. Furthermore for practical application, a compen-sating method is given when the theoretical scaled actuators or sensors cannot be obtained. Also, the scaling laws of some non-linear elements in control system such as the rate and amplitude sat-urations in actuator have been studied and examined by a numerical simulation. 相似文献
688.
Kai Ning Baolin Wu Chuang Xu 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2021,67(6):1761-1772
The problem of attitude takeover control of spacecraft by using cellular satellites with limited communication, actuator faults and input saturation is investigated. In order to lighten the communication burden of cellular satellites, an event-triggered control strategy is adopted. The filtered attitude information needs to be transmitted only when the defined measurement error reaches the event-triggered threshold in this strategy. Then, to deal with the unknown inertia matrix, actuator faults, external disturbances and the errors caused by event-triggered scheme, fuzzy logic systems is introduced to estimate the uncertainties directly. Combining fuzzy logic control strategy and the event-triggered method, the first event-triggered adaptive fuzzy control law is developed. Then, torque saturation of cellular satellites is further considered in the second control law, where the upper bound of the uncertainties is estimated by fuzzy logic systems. The resulting closed-loop systems under the two control laws are guaranteed to be bounded. Finally, the effectiveness of two proposed control laws is verified by the numerical simulations. 相似文献
689.
《中国航空学报》2021,34(5):341-349
Aviation products would go through a multi-phase improvement in reliability performance during the research and development process. In the literature, most of the existing reliability growth models assume a constant failure intensity in each test phase, which inevitably limits the scope of the application. To address this problem, we propose two new models considering time-varying failure intensity in each stage. The proposed models borrow the idea from the accelerated failure-time models. It is assumed that time between failures follow the log-location-scale distribution and the scale parameters in each phase do not change, which forms the basis for integrating the data from all test stages. For the test-find-test scenario, an improvement factor is introduced to construct the relationship between two successive location parameters. Whereas for the test-fix-test scenario, the instantaneous cumulative time between failures is assumed to be consistent with Duane model and derive the formulation of location parameter. Likelihood ratio test is further utilized to test whether the assumption of constant failure intensity in each phase is suitable. Several applications with real reliability growth data show that the assumptions are reasonable and the proposed models outperform the existing models. 相似文献
690.
研究了多回路法场路耦合算法的基本原理,为了提高系统的仿真效率,对联合仿真中的迭代模式、分布式仿真进行了讨论。在此基础上,采用该算法对某三级无刷交流电源系统的典型极端故障工况进行了仿真分析。仿真结果表明,基于多回路场路耦合的联合仿真算法具有良好的数值收敛性,能有效对供电系统的稳态、瞬态以及故障状态进行分析。 相似文献