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Feasibility study of the beating cancellation during the satellite vibration test

机译:卫星振动测试中消除跳动的可行性研究

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摘要

The difficulties of satellite vibration testing are due to the commonly expressed qualification requirements being incompatible with the limited performance of the entire controlled system (satellite + interface + shaker + controller). Two features cause the problem: firstly, the main satellite modes (i.e., the first structural mode and the high and low tank modes) are very weakly damped; secondly, the controller is just too basic to achieve the expected performance in such cases. The combination of these two issues results in oscillations around the notching levels and high amplitude beating immediately after the mode. The beating overshoots are a major risk source because they can result in the test being aborted if the qualification upper limit is exceeded. Although the abort is, in itself, a safety measure protecting the tested satellite, it increases the risk of structural fatigue, firstly because the abort threshold has been already reached, and secondly, because the test must restart at the same close-resonance frequency and remain there until the qualification level is reached and the sweep frequency can continue. The beat minimum relates only to small successive frequency ranges in which the qualification level is not reached. Although they are less problematic because they do not cause an inadvertent test shutdown, such situations inevitably result in waiver requests from the client. A controlled-system analysis indicates an operating principle that cannot provide sufficient stability: the drive calculation (which controls the process) simply multiplies the frequency reference (usually called cola) and a function of the following setpoint, the ratio between the amplitude already reached and the previous setpoint, and the compression factor. This function value changes at each cola interval, but it never takes into account the sensor signal phase. Because of these limitations, we firstly examined whether it was possible to empirically determine, using a series of tests with a very simple dummy, a controller setting process that significantly improves the results. As the attempt failed, we have performed simulations seeking an optimum adjustment by finding the Least Mean Square of the difference between the reference and response signal. The simulations showed a significant improvement during the notch beat and a small reduction in the beat amplitude. However, the small improvement in this process was not useful because it highlighted the need to change the reference at each cola interval, sometimes with instructions almost twice the qualification level. Another uncertainty regarding the consequences of such an approach involves the impact of differences between the estimated model (used in the simulation) and the actual system. As limitations in the current controller were identified in different approaches, we considered the feasibility of a new controller that takes into account an estimated single-input multi-output (SIMO) model. Its parameters were estimated from a very low-level throughput. Against this backdrop, we analyzed the feasibility of an LQG control in cancelling beating, and this article highlights the relevance of such an approach.
机译:卫星振动测试的困难是由于通常表达的资格要求与整个受控系统(卫星+接口+振动台+控制器)的有限性能不兼容。造成此问题的原因有两个:首先,主要的卫星模式(即第一结构模式和高低坦克模式)被非常弱地衰减;其次,在这种情况下,控制器太基本了,无法达到预期的性能。这两个问题的结合会导致陷波水平附近出现振荡,并在模式之后立即出现高振幅跳动。跳动超调是主要的风险来源,因为如果超出资格上限,它们可能导致测试中止。尽管中止本身就是保护被测试卫星的安全措施,但它增加了结构疲劳的风险,首先是因为已经达到中止阈值,其次是因为测试必须以相同的近共振频率重新开始,并且保持在那里直到达到鉴定级别并且扫描频率可以继续。最小拍频仅与未达到合格级别的较小连续频率范围有关。尽管它们的问题较少,因为它们不会导致意外的测试关闭,但这种情况不可避免地会导致来自客户端的放弃请求。受控系统分析表明操作原理无法提供足够的稳定性:驱动计算(控制过程)仅将频率参考(通常称为可乐)与以下设定值的函数相乘,即已达到的振幅与先前的设定点和压缩系数。该功能值在每个可乐间隔内都会变化,但是它永远不会考虑传感器信号的相位。由于这些限制,我们首先检查了是否有可能通过使用非常简单的虚拟模型进行一系列测试来凭经验确定控制器设置过程,从而显着改善结果。由于尝试失败,我们进行了仿真,通过找到参考信号和响应信号之间的差异的最小均方来寻求最佳调整。仿真显示陷波节拍期间有显着改善,节拍幅度有小幅下降。但是,此过程中的小幅改进没有用,因为它突出显示了在每个可乐间隔中更改参考的必要性,有时使用的指示几乎是鉴定水平的两倍。关于这种方法的后果的另一个不确定性涉及估计模型(用于仿真)和实际系统之间差异的影响。由于以不同的方法确定了当前控制器的局限性,因此我们考虑了考虑估计的单输入多输出(SIMO)模型的新型控制器的可行性。它的参数是从非常低的吞吐量估算出来的。在此背景下,我们分析了LQG控件在消除跳动中的可行性,并且本文重点介绍了这种方法的相关性。

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