Determination of elastic mode characteristics using wirelessly networked sensors for nanosat launch vehicle control

Ramin Rezaei, Fady Ghabrial, E. Besnard, P. Shankar, Joel Castro, Lonnie Labonte, Mojtaba Razfar, A. Abedi
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引用次数: 1

Abstract

This paper presents a simulation study of the realtime determination of the elastic mode characteristics (frequency and displacement mode shape) of a launch vehicle using an array of sensors that measure the local strain along the length of the vehicle. The determination of the frequency and shape of the excited modes is accomplished using the buffered strain data. We assume that the sensed data is obtained from a wirelessly networked array of sensors that brings in additional complexity due to the presence of delays, packet loss and network dynamics. Preliminary results show a high sensitivity of the mode-shape determination algorithm to delays in sensed information.
基于无线网络传感器的纳米卫星运载火箭控制弹性模态特性测定
本文提出了一种利用传感器阵列实时测定运载火箭弹性模态特性(频率和位移模态形状)的仿真研究,该传感器阵列测量沿运载火箭长度方向的局部应变。利用缓冲应变数据确定了激发态的频率和形状。我们假设感测数据是从无线网络传感器阵列中获得的,由于存在延迟、数据包丢失和网络动态,这带来了额外的复杂性。初步结果表明,该算法对感知信息的延迟具有较高的灵敏度。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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