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A Hybrid Model using Genetic Algorithm for Energy Optimization in Heterogeneous Internet of Blockchain Things (IoBT) 基于遗传算法的异构区块链物联网能源优化混合模型
Pub Date : 2023-01-01 DOI: 10.1615/telecomradeng.2023050237
Mahesh Babu Ravi, krishna Prasad Satamraju, Neeharika Gangothri Bellagubbala, Malarkodi Balakrishnan, Venkata Suresh Chintalapudi
Internet of Things (IoT) emerging is one of the promising technologies aspiring industries and public alike with its broad spectrum of applications adding intelligence to the real-life objects. Due to its resource-limited nature, and heterogeneity of the devices in IoT networks, data security and energy consumption is a burning issue. Security for sensitive data in the network is paramount and privacy and access control mechanisms should be in force. Also, for reliable application services, the optimized network operations in terms of energy are demanding needs nowadays. This paper proposed a novel energy optimization and node deployment strategy is proposed by amalgamating genetic algorithm (GA) for energy optimization and mixed integer linear programming (MILP) for strategic node replacement. GA-based optimization focuses on improving residual energy of the nodes in the network thereby enhancing the network life-time. The MILP based node deployment strategy focuses on selecting minimum node set while still servicing the entire network area. The potentiality of the Blockchain is used in the model to provide data privacy and access control to the sensitive data. The proposed model is then compared with the state-of-the-art models to validate the performance in terms of network life-time, and throughput. It is evident from the results that the proposed method outperforms the existing models and provides reliable and viable solutions for many applications running on the IoT networks
物联网(IoT)新兴是有抱负的行业和公众都喜欢的有前途的技术之一,其广泛的应用为现实生活中的物体增加了智能。由于其资源有限的性质,以及物联网网络中设备的异构性,数据安全和能耗是一个亟待解决的问题。网络中敏感数据的安全至关重要,隐私和访问控制机制应该生效。此外,为了提供可靠的应用服务,优化的网络运行在能源方面也是当今的需求。将遗传算法(GA)用于能量优化和混合整数线性规划(MILP)用于战略性节点替换相结合,提出了一种新的能量优化和节点部署策略。基于遗传算法的优化侧重于提高网络中节点的剩余能量,从而提高网络的寿命。基于MILP的节点部署策略侧重于选择最小节点集,同时仍然服务于整个网络区域。该模型利用区块链的潜力,为敏感数据提供数据隐私和访问控制。然后将建议的模型与最先进的模型进行比较,以在网络生命周期和吞吐量方面验证性能。从结果中可以明显看出,所提出的方法优于现有模型,并为在物联网网络上运行的许多应用提供了可靠和可行的解决方案
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引用次数: 0
Mathematical Modeling Methods in Designing Onboard Laser-Ranging Systems of Spacecraft 航天器机载激光测距系统设计中的数学建模方法
Pub Date : 2021-11-09 DOI: 10.36027/rdeng.0321.0000195
E. I. Starovoitov, D. Savchuk
To perform rendezvous and docking of spacecraft (SC), it is necessary to detect and measure the coordinates of a passive space vehicle (SV) using the onboard aids of an active SV. For this purpose, in addition to radio engineering systems, laser-ranging systems (LRS) are used. A designing process of the onboard LRS for promising spacecraft is currently becoming more complicated and requires taking into account a lot of factors.The authors have developed the PC software to assess capabilities of onboard pulse LRS of spacecraft when working on the nearby or distant space objects that have a diffusely scattering surface, as well as are equipped with the corner reflectors. The software also allows us to calculate the LRS parameters, which, according to GOST R 50723-94, ensure eye-safety in the spectral range of 0.81 ... 1.5 microns in case of accidental irradiation.The energy of the intensifier pulse and the divergence of a sensing beam determine the LRS range and the distance of eye-safe observation, which are the most important indicators to characterize the onboard LRS capabilities. To ensure the best LRS range and safety characteristics simultaneously, it is necessary to solve the problem of multi-criteria optimization.The paper solves the problem of multi-criteria optimization for the maximum LRS range and the eye-safe observation distance by Pareto sets the use of which allows us to avoid uncertainty in choosing a significance of criteria.The results obtained show that the proposed methods can be successfully applied in designing onboard LRS of spacecraft.
为了实现航天器的交会对接,需要利用主动航天器的机载辅助对被动航天器的坐标进行探测和测量。为此,除了无线电工程系统外,还使用激光测距系统(LRS)。未来航天器机载LRS的设计过程越来越复杂,需要考虑很多因素。作者开发了一种PC软件,用于评估航天器机载脉冲LRS在近距离或远距离具有扩散散射表面的空间物体上工作时的能力,并配备了角反射器。该软件还允许我们计算LRS参数,根据GOST R 50723-94,在0.81…1.5微米,以防意外辐照。增强器脉冲的能量和感应光束的发散度决定了LRS的距离和眼安全观测距离,这是表征机载LRS能力的最重要指标。为了同时保证最佳的LRS范围和安全特性,需要解决多准则优化问题。利用Pareto集解决了最大LRS距离和人眼安全观测距离的多准则优化问题,利用Pareto集避免了准则显著性选择的不确定性。结果表明,该方法可以成功地应用于星载LRS的设计。
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引用次数: 0
Odd Mathieu Functions Application to Synthesize a Multi-element Radiator Flat-topped Radiation Pattern 奇Mathieu函数在多单元辐射体平顶辐射图合成中的应用
Pub Date : 2021-11-09 DOI: 10.36027/rdeng.0321.0000194
Y. Rusov, A. Propastin
The paper studies synthesizing capabilities of a flat-topped radiation pattern when using the expansion of the target radiation pattern into a series in terms of odd Mathieu functions. As parameters for comparing the target and synthesized radiation patterns, we used a main-lobe width at a level of -1 dB and an irregularity of the top of the main-lobe of the radiation pattern. The sector-shaped radiation pattern has been synthesized for linear radiators of various lengths. The convergence of the coefficients of the Mathieu series in the synthesis of the sector-shaped radiation pattern has been estimated. It is shown that the use of piecewise-linear approximation of the target radiation pattern in the synthesis using a series expansion into odd Mathieu functions allows us to improve the quality of the radiation pattern formed.The task that involved finding the amplitude-phase distribution for a linear emitter with a length of 3λ, 4λ and 5λ (λ is operation wavelength) for a target radiation pattern was solved. The target amplitude distribution has the following electrical characteristics: the main-lobe width is 37.5° at a level of -1 dB and the side lobe level (SLL) is -20 dB. The synthesis procedure was performed for two cases. In the first case, the target radiation pattern is represented by a piecewise constant function with a given width. In the second case, the target pattern was specified using piecewise linear approximation of the top and slopes of the main lobe.Comparison of the radiation patterns obtained shows that in the first case, the main-lobe width of the radiation pattern at a level of -1 dB is 34°, the SLL varies from -15.6 to -17 dB, and the irregularity of the main-lobe top of the radiation pattern lies within 0.9 ... 1.2 dB. In the second case, the main-lobe width of the antenna radiation pattern at a level of -1 dB is 36.5°, the SLL is -17.5 dB, and the irregularity of the main-lobe top is 0.4 dB at most. When used, the considered under consideration enables us to obtain both the synthesized patterns for linear radiators of various lengths, and the corresponding amplitude-phase distributions and coefficients of the Mathieu series. An estimate of the convergence of the Mathieu series shows that the use of linear approximation of the target radiation pattern in some cases allows up to 2.7-fold increase in acceleration of the convergence of the Mathieu series. The accuracy of reproducing the sector-shaped pattern by the synthesis method using the expansion into odd Mathieu functions gives good results when synthesizing the amplitude-phase distribution for the linear radiators with an electric length of 5λ or more.
本文研究了将目标辐射方向图展开成奇马修函数级数时平顶辐射方向图的综合能力。作为比较目标和合成辐射图的参数,我们使用了-1 dB水平的主瓣宽度和辐射图主瓣顶部的不规则度。对不同长度的线性辐射体合成了扇形辐射图。估计了扇形辐射图合成中Mathieu级数系数的收敛性。结果表明,将目标辐射方向图的分段线性近似用级数展开成奇马蒂厄函数,可以提高所形成的辐射方向图的质量。求解了长度为3λ、4λ和5λ (λ为工作波长)的线性发射器的幅相分布问题。目标振幅分布具有以下电特性:主瓣宽度为37.5°,电平为-1 dB,副瓣电平(SLL)为-20 dB。对两种情况进行了合成。在第一种情况下,目标辐射方向图由具有给定宽度的分段常数函数表示。在第二种情况下,使用主瓣的顶部和斜率的分段线性逼近来指定目标图案。对比得到的辐射图可知,第一种情况下,-1 dB水平处的辐射图主瓣宽度为34°,SLL变化范围为-15.6 ~ -17 dB,辐射图主瓣顶部的不规则性在0.9 ~ 17 dB之间。1.2 dB。在第二种情况下,天线辐射方向图在-1 dB电平处的主瓣宽度为36.5°,SLL为-17.5 dB,主瓣顶部的不规则性最大为0.4 dB。当使用所考虑的时侯,我们既可以得到不同长度的线性辐射体的合成图,也可以得到相应的Mathieu级数的幅相分布和系数。对Mathieu级数收敛性的估计表明,在某些情况下,使用目标辐射方向图的线性近似可以使Mathieu级数的收敛速度提高2.7倍。对于电长大于等于5λ的线性辐射体,利用奇Mathieu函数展开法合成扇形图的精度较高。
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引用次数: 0
Information-Measuring Complex to Detect High Frequency Gravitational Waves 探测高频引力波的信息测量复合体
Pub Date : 2021-08-22 DOI: 10.36027/rdeng.0221.0000190
I. Golyak, A. Morozov, A. L. Nazolin, S. E. Tabalin, A. Esakov, I. Fomin
The gravitational waves predicted by the general theory of relativity and detected by the Laser Interferometer Gravitational-wave Observatory (LIGO) have typical frequencies in the range of 30 ... 300 Hz. Current theories of gravity predict the existence of high-frequency gravitational waves with frequencies of 10 ... 100 MHz, including those of cosmological origin, induced by quantum fluctuations of the scalar field at the stage of cosmological inflation in the early Universe.Multi-beam optical resonators, in particular the Fabry-Perot interferometers, can be used to detect high-frequency gravitational waves. When using multi-beam optical resonators, it is possible to use the phenomenon of low-frequency optical resonance, which allows us to have a selective response to the gravitational wave effect. The gravitational-optical resonance in a multi-beam interferometer occurs if the condition is fulfilled that an integer number of half-waves of gravitational radiation is along the length of the resonator.The use of a multi-beam interferometer to detect high-frequency gravitational waves does not require the creation of a complex system for decoupling mirrors used for gravitational antennas operating in the low-frequency part of the spectrum. This is due to the fact that the frequency of mechanical vibrations of the interferometer mirrors is significantly less than the frequency of the gravitational wave.The paper considers possible optical schemes of a high-frequency gravitational antenna: based on the traditional Michelson interferometer, in the arms of which two Fabry-Perot interferometers are available, and on the basis of the Mach-Zehnder optical scheme, where Fabry-Perot interferometers can be made in the form of two perpendicular arms, with reflecting mirrors at the bend of the beam. The advantage of the second scheme is that three photo-detectors, one being main and two others being auxiliary, can be used, and there is a possibility to detect radiation transmitted by Fabry-Perot interferometers.To prove that detection of high-frequency gravitational waves is possible, a potential sensitivity of the high-frequency gravitational antenna has been estimated in the paper.
广义相对论预测的引力波和激光干涉仪引力波天文台(LIGO)探测到的引力波的典型频率在30…300赫兹。目前的重力理论预测存在频率为10的高频引力波。100兆赫,包括宇宙起源的那些,在宇宙早期宇宙膨胀阶段由标量场的量子涨落引起。多光束光学谐振器,特别是法布里-珀罗干涉仪,可以用来探测高频引力波。在使用多光束光学谐振器时,可以利用低频光学谐振现象,使我们对引力波效应有选择性的响应。在多光束干涉仪中,如果满足沿谐振腔长度方向存在一定数量的引力辐射半波的条件,就会产生引力光共振。使用多波束干涉仪探测高频引力波,不需要为在低频部分工作的引力天线创建一个复杂的解耦镜系统。这是由于干涉仪反射镜的机械振动频率明显小于引力波的频率。本文考虑了高频重力天线可能的光学方案:基于传统的迈克尔逊干涉仪(臂上有两个法布里-珀罗干涉仪)和基于马赫-曾德尔光学方案(法布里-珀罗干涉仪可以制成两个垂直臂,在光束的弯曲处有反射镜)。第二种方案的优点是可以使用三个光电探测器,一个是主探测器,另外两个是辅助探测器,并且有可能探测到由法布里-珀罗干涉仪传输的辐射。为了证明探测到高频引力波是可能的,本文对高频引力波天线的潜在灵敏度进行了估计。
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引用次数: 0
Investigation of Aerosol Inhomogeneities Parameters in Planetary Boundary Layer in UV-A Spectral Region 紫外- a光谱区行星边界层气溶胶不均匀性参数的研究
Pub Date : 2021-05-30 DOI: 10.36027/rdeng.0121.0000187
P. A. Filimonov, S. Ivanov, V. Gorodnichev, M. L. Belov, Y. Fedotov
For today necessity of atmosphere wind remote sensing for wide pool of applications require development of new measurement methods and improvement of already existing.Currently doppler methods for wind speed measuring have largest sensing range. Correlation-based methods are provide lower sensing range for wind speed measurement. However, doppler-based lidar are expensive in opposite to simply designed correlation lidars that additionally allows to measure wind profile along sensing direction.Development of wind correlation lidars required knowledge of atmosphere aerosol inhomogeneities parameters.The most experimental research till now in this area are related to visible spectral range.One of the perspective eye-safety spectral range for wind lidar is UV spectral region. There not so much experimental research works of aerosol inhomogeneities parameters in UV.This paper is related to field experiments of aerosol inhomogeneities parameters in planetary boundary layer on 0.355 um operating wavelength.Block diagram and parameters of lidar with 0.355 operating wavelength is shown. Process of experiments is described. Typical atmosphere backscattering echo-signal for single laser pulse is demonstrated.Procedures if lidar signals processing are described, example of two-dimensional field of relative fluctuations of volume backscattering coefficient for different atmosphere conditions is shown.Results of measurement data processing shown that in planetary boundary layer average contrast of aerosol inhomogeneities in most cases has values in range 0,4% – 10 % (in case of snow up to 25%), and size in range 1,5 – 20 m. Dependency of observation number of aerosol inhomogeneities by range z from lidar to backscattering volume is descending with 1/z manner that the same for dependency for signal-noise ratio SNR(z).
由于大气风遥感的广泛应用,需要开发新的测量方法和改进现有的测量方法。目前多普勒风速测量方法的传感范围最大。基于相关的方法为风速测量提供了较低的传感范围。然而,基于多普勒的激光雷达价格昂贵,与简单设计的相关激光雷达相反,后者可以沿着传感方向测量风廓线。发展风相关激光雷达需要了解大气气溶胶不均匀性参数。迄今为止,该领域的实验研究大多与可见光谱范围有关。紫外光谱区是风激光雷达对人眼安全的透视光谱范围之一。紫外辐射下气溶胶非均质性参数的实验研究并不多。本文对行星边界层在0.355 um工作波长上的气溶胶不均匀性参数进行了野外实验研究。给出了工作波长为0.355的激光雷达的框图和参数。描述了实验过程。给出了典型的单激光脉冲大气后向散射回波信号。描述了激光雷达信号的处理过程,给出了不同大气条件下体积后向散射系数相对波动的二维场实例。测量数据处理的结果表明,在大多数情况下,在行星边界层中,气溶胶不均匀性的平均对比值在0.4% - 10%范围内(在积雪高达25%的情况下),大小在1.5 - 20 m范围内。激光雷达波段气溶胶非均匀性观测数与后向散射体积的相关性呈1/z递减,信噪比SNR(z)的相关性也呈1/z递减。
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引用次数: 0
Research of the Possibilities of Matching the Multi-element Receiving-Transmitting Irradiator Aperture 多单元收发辐射器孔径匹配的可能性研究
Pub Date : 2021-05-30 DOI: 10.36027/rdeng.0121.0000168
Y. Rusov, S. S. Krapivina
Currently, aperture antennas with spatial excitation, such as reflector antennas and phased array antennas, are widely used in radar. The composition of such an antenna includes an irradiator, which can be made in the form of a small-element array of radiators to form a set of necessary radiation patterns. Monopulse irradiators are often used, which form both total and difference directional patterns. When performing an irradiator based on waveguide parts, radiators in the form of horns or open ends of waveguides are installed in its aperture. Waveguide irradiators with four and twelve horns are widely used. One of the main electrical characteristics of such an irradiator when used as part of a receiving-transmitting antenna is the isolation of the transmitting and receiving paths. Matching the aperture of the transmitting and receiving irradiator has a significant effect on the isolation of its waveguide channels. With small transverse dimensions of the radiators in the form of open ends of waveguides, it is not possible to obtain high isolation of waveguide channels without the use of additional matching elements. The task of research the effect of matching the aperture of a waveguide multi-element irradiator on the isolation of its transmitting and receiving channels, as well as the ways of matching its radiators, is set.The article considers a four-horn irradiator, the aperture of which contains radiators in the form of open ends of a square waveguide. Each radiator has the radius rounding required for the manufacture of the product using the available technological processes. To match the emitter, a dielectric plate is installed inside it. During the research the thickness of the plate and its location relative to the aperture plane changed. The characteristics of matching the radiators with a plate made of teflon, polyethylene and ST-4 material based on polymers filled with titanium dioxide are presented.The proposed method of matching the opening of a multi-element irradiator with a transverse emitter size of 0,68λ (λ is the wavelength in free space corresponding to the average frequency of the operating band) makes it possible to improve the isolation of the receiving and transmitting waveguide channels by at least 4 dB in the frequency band of up to 3%.
目前,具有空间激励的孔径天线,如反射面天线和相控阵天线,在雷达中得到了广泛的应用。该天线的组合物包括辐照体,该辐照体可制成辐照体的小元件阵列的形式,以形成一组必要的辐射图案。通常使用单脉冲辐射器,它可以形成全方向和差方向。当使用基于波导部件的辐照器时,在其孔径内安装角状或波导开口端的散热器。四角和十二角波导辐射器被广泛使用。当用作收发天线的一部分时,这种辐照器的主要电气特性之一是发射和接收路径的隔离。发射和接收辐射体孔径的匹配对其波导通道的隔离有重要影响。由于辐射体的横向尺寸较小,以波导开口端的形式存在,如果不使用额外的匹配元件,就不可能获得波导通道的高度隔离。本文的任务是研究波导多单元辐射器孔径匹配对其发射和接收通道隔离的影响,以及其辐射器的匹配方式。本文考虑了一个四角辐照器,其孔径包含方形波导开口端形式的辐照器。每个散热器都具有使用可用技术工艺制造产品所需的半径。为了与发射极相匹配,在其内部安装了一个介电板。在研究过程中,平板的厚度及其相对于孔径平面的位置发生了变化。介绍了以聚四氟乙烯、聚乙烯和ST-4材料为基材,以二氧化钛填充聚合物为基材的散热器配板的特点。所提出的将多元件辐照体的开口与横向发射器尺寸为0.68 λ (λ为与工作频带平均频率相对应的自由空间中的波长)相匹配的方法使得在高达3%的频带内将接收和发射波导通道的隔离度提高至少4db成为可能。
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引用次数: 0
Glycerin-containing Working Fluids for Hydraulic Drives for Special Purposes 特殊用途液压传动用含甘油工作液
Pub Date : 2020-12-26 DOI: 10.36027/rdeng.0620.0000182
K. D. Efremova, V. Pilgunov
The cavitation properties of a liquid must be taken into account in the engineering design of hydraulic machines and devices for hydraulic automation in cases when in their working process the absolute pressure in the liquid may drop below atmospheric, and the liquid is in a rarefied state for a certain time. Cold boiling, which occurs at a relatively low temperature and reduced absolute pressure inside or on the surface of the liquid, is considered as hydrostatic cavitation, if the liquid is stationary, or as hydrodynamic cavitation, if the liquid enters conditions under which the velocity head sharply increases in the flow section and the absolute pressure.In accordance with the theory of cavitation, the first phase of cavitation occurs when the absolute pressure in the degassed liquid drops to the value of the saturated vapor pressure and the air dissolved in the liquid, leaving the intermolecular space, turns into microbubbles of undissolved air and becomes a generator of cavitation "nuclei". Of practical interest is a quantitative assessment of the value of the minimum permissible absolute pressure in a real, partially or completely degassed liquid, at which hydrostatic cavitation occurs.Since the pressure of saturated vapor of a liquid is, to a certain extent, associated with the forces of intermolecular interaction, it is necessary to have information on the cavitation properties of technical solutions, including the solution of air in a liquid, since a solute can weaken intermolecular bonds and affect the value of the pressure of saturated vapors of the solvent. The article describes an experiment carried out by the authors to evacuate liquids. During the experiment, evacuation of various liquids was carried out using a developed hydraulic vacuum pump with a pneumatic drive.The article presents the technologies of hydrostatic and hydrodynamic degassing of liquids used in the experiment.As a result of experimental studies of the cavitation properties of pure glycerin and glycerin in the form of a 49/51% solution in water, mineral oil and aviation kerosene, quantitative estimates of the permissible absolute pressure in the considered technical fluids and solutions were obtained, its dependence on the saturated vapor pressure, the influence of the degree of hydrodynamic degassing the liquid, and the amount of dissolved substance in it on the strength of the liquid to rupture.In the process of studying the cavitation properties of solutions, it was found that the level of permissible absolute pressure in the solution is greater than that of the solvent. It has been suggested that dissolved solid, liquid or gaseous substances weaken the intermolecular bonds of the solvent and increase the pressure of its saturated vapor.On the basis of the experimental studies, a method for determining the highest rarefaction in solvents and in glycerol solutions has been developed. In addition, a comparative assessment of the cavitation properties of the cons
当液体在工作过程中绝对压力可能降到大气压以下,且液体在一定时间内处于稀薄状态时,在液压自动化用液压机和装置的工程设计中必须考虑液体的空化特性。冷沸腾发生在温度相对较低,液体内部或表面的绝对压力降低的情况下,如果液体是静止的,则称为静水空化;如果液体进入流段速度头和绝对压力急剧增加的情况,则称为动水空化。根据空化理论,当脱气液体中的绝对压力下降到饱和蒸汽压时,溶解在液体中的空气离开分子间空间,变成未溶解空气的微泡,成为空化“核”的产生器时,就会发生第一阶段的空化。有实际意义的是定量评估在发生流体静力空化时,部分或完全脱气的实际液体中允许的最小绝对压力的值。由于液体饱和蒸汽的压力在一定程度上与分子间相互作用的力有关,因此有必要了解技术溶液(包括空气在液体中的溶液)的空化特性,因为溶质可以削弱分子间键并影响溶剂饱和蒸汽的压力值。这篇文章描述了作者进行的一项排出液体的实验。在实验过程中,使用一种开发的液压真空泵与气动驱动进行各种液体的疏散。本文介绍了实验中采用的流体静力和流体动力脱气技术。通过对纯甘油和甘油在水、矿物油和航空煤油中49/51%溶液形式的空化特性的实验研究,获得了所考虑的技术流体和溶液中允许的绝对压力的定量估计,其对饱和蒸汽压的依赖,流体动力脱气程度的影响,以及其中溶解物质的数量对液体破裂强度的影响。在研究溶液空化特性的过程中,发现溶液中的允许绝对压力水平大于溶剂的允许绝对压力水平。有人认为,溶解的固体、液体或气体物质削弱了溶剂的分子间键,增加了其饱和蒸气的压力。在实验研究的基础上,建立了测定溶剂和甘油溶液中最高稀度的方法。此外,还对所考虑的技术流体的空化特性进行了比较评价。
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引用次数: 0
Navigation Support for Monitoring the Underlying Surface From UAV with a Passive Optical Sensor 无源光学传感器对无人机下垫面监测的导航支持
Pub Date : 2020-12-25 DOI: 10.36027/RDENG.0520.0000183
E. I. Starovoytov
На сегодняшний день с помощью беспилотных летательных аппаратов (БПЛА) решается широкий круг задач, в том числе мониторинг окружающей среды и обследование зон чрезвычайных ситуаций, при которых выполняется локация различных объектов на подстилающей поверхности и их последующая привязка к географическим координатам.Развитие беспилотных систем в настоящее время тесно связано с оптическими датчиками, используемыми на БПЛА всех типов. Пассивные оптические датчики имеют малые массу и габариты, потребляют небольшую мощность от бортовой сети электропитания, при этом они могут измерять дальности до объектов со сложной конфигурацией и ненормированным коэффициентом отражения поверхности.Цель данной работы – анализ требований к навигационной аппаратуре при измерении дальности монокулярным пассивным оптическим датчиком до статических наземных объектов с борта БПЛА и их последующей привязке к географическим координатам.Выполнены оценки разных вариантов осуществления оптической локации наземных объектов параллаксным методом измерений с оптической и навигационной аппаратурой на борту легких БПЛА малого радиуса действия, мини- и микро-БПЛА. В качестве источников навигационных данных может быть использована аппаратура спутниковой навигации, телекамеры, бесплатформенная инерциальная навигационная система, барометрический высотомер и цифровой компас.При использовании рассматриваемых навигационных датчиков обеспечивается измерение дальностей до 1000 м с относительной погрешностью не более 10 %. При привязке объектов к географическим координатам оценки погрешности как для прямолинейной, так и для сложной траектории полета БПЛА различаются не более чем на 4,1 м для всех типов навигационных датчиков, а позиционная ошибка не превышает 150 м при величине ошибки по высоте не более 40 м.В ранее известных работахоценка измерений выполнялась на малом базисе (уход БИНС не учитывался), а привязка обнаруженных объектов к географическим координатам не выполнялась.Результаты работы могут применяться в разработке навигационных систем различных БПЛА и беспилотных систем мониторинга наземной обстановки.
迄今为止,无人驾驶飞机(无人机)解决了广泛的任务,包括环境监测和紧急情况调查,以确定不同物体在地面上的位置和随后与地理坐标的联系。无人机系统的发展与各种类型无人机上使用的光学传感器密切相关。被动光学传感器的质量和大小小,从机载电网消耗小功率,可以测量距离到具有复杂配置和异常表面反射系数的物体。这项工作的目的是分析导航设备的要求,将单眼被动光学传感器测量到无人机上的静态地面物体,并将其与地理坐标联系起来。对地面物体的不同光学位置进行了评估,视差测量方法包括小范围轻型无人机、微型和微型无人机。卫星导航设备、电视摄像机、免费惯性导航系统、气压计高度表和数字罗盘可以作为导航的来源。在使用这些导航传感器时,可以测量多达1000米的距离,但相对误差不超过10%。地理坐标误差评估挂钩的物体时对于直线轨迹和复杂的无人机区分不超过4.1 m为各类导航传感器,定位误差不超过1.5 m的大小高度误差不超过40м.В前身работахоценк维度基础上执行(离开beans忽略),探测物体盯住地理坐标没有听从。结果可以应用于开发各种无人机和地面监测系统的导航系统。
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引用次数: 0
Information-Measuring Complex for Registration High Frequency Gravitational Waves 高频引力波配准信息测量复合体
Pub Date : 2020-12-25 DOI: 10.36027/rdeng.0520.0000184
I. Golyak, A. Morozov, A. L. Nazolin, S. E. Tabalin
The information-measuring complex designed to register high-frequency fluctuations of the space-time metric and its main elements are described in paper. The complex is based on a Fabry-Perot interferometer with highly reflective mirrors and a two-meter resonator. A solid-state Nd: YAG laser with a wavelength λ = 1064 nm is used for pumping. To read the signal, an InGaAs receiver DET10N2, with a working spectral range of 500-1700 nm and an active region of 0.8 mm2, is applied. Using the developed complex, experimental studies of signal registration at readout frequencies of 1 MHz and 20 MHz were carried out. The graphs of signal fluctuations in time and the spectra constructed from them are given.
本文介绍了用于记录时空度量高频波动的信息测量复合体及其主要元件。该综合体基于一个具有高反射镜和一个两米谐振器的法布里-珀罗干涉仪。利用波长λ = 1064 nm的Nd: YAG固态激光器进行泵浦。为了读取信号,使用了一个InGaAs接收器DET10N2,其工作光谱范围为500-1700 nm,有源区域为0.8 mm2。利用开发的复合体,进行了1 MHz和20 MHz读出频率下信号配准的实验研究。给出了信号随时间波动的图及其构成的谱。
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引用次数: 2
Analysis of the Possibility of Remote Laser Detection of Propane Leaks 激光远程检测丙烷泄漏的可能性分析
Pub Date : 2020-12-25 DOI: 10.36027/RDENG.0520.0000185
M. L. Belov, K. S. Titarenko, V. Gorodnichev
Propane is one of the main components of the wide fraction of light hydrocarbons (WLHF). A large volume of WLHF is transported to petrochemical plants via pipelines. Control of pipelines is carried out by means of in-line pressure sensors. However, they are ineffective for detecting low-intensity leaks.To detect low-intensity propane leaks from pipelines, it is promising to use a remote laser gas analyzer installed on an aircraft.The article is devoted to the analysis of the possibilities of remote laser detection of propane leaks.Based on the data on the absorption of propane and atmospheric gases, the wavelengths of 3370 nm (in the maximum absorption of propane) and 3550 nm (in the spectral region where there is no absorption of propane) were chosen as the sounding wavelengths.It was believed that the monitoring of propane leaks is carried out by a lidar installed on the aircraft in a monostatic sensing scheme. The method of differential absorption with scattering from the earth's surface is used.To detect propane leaks, an information parameter was used, which is equal to the ratio of the power recorded by the receiver at wavelengths of 3370 nm and 3550 nm. The value of the information parameter was calculated for different heights of the propane layer on the earth's surface and different concentrations of propane in the layer.Statistical modeling was performed to quantify the effectiveness of remote detection of propane leaks.In the work, the probability of correct detection of a propane leak (detection of a leak when it is in reality) and the probability of false alarms (detection of a leak when it is not in reality) were calculated.The decision to detect propane leaks was made when the value of the information parameter was less than the threshold.The results of mathematical modeling show that for a propane content in the leak of at least 0.17 % (an order of magnitude less than the concentration limit of flame propagation), the problem of remote detection of propane leaks from the pipeline can be solved with a probability of correct detection of more than 0.999 and a probability of false alarms of less than 0.001 with a thickness of the propane layer on the earth's surface of at least 20 cm.
丙烷是宽馏分轻烃(WLHF)的主要组分之一。大量废液通过管道输送到石化厂。管道的控制是通过在线压力传感器来实现的。然而,它们对于检测低强度泄漏是无效的。为了检测管道中的低强度丙烷泄漏,有希望使用安装在飞机上的远程激光气体分析仪。本文分析了激光远程检测丙烷泄漏的可能性。根据对丙烷和大气气体的吸收数据,选择了3370 nm(丙烷的最大吸收波长)和3550 nm(没有丙烷吸收的光谱区域)作为探测波长。据信,丙烷泄漏的监测是由安装在飞机上的激光雷达以单源传感方案进行的。采用了地球表面散射微分吸收的方法。为了检测丙烷泄漏,使用了一个信息参数,该参数等于接收器在3370 nm和3550 nm波长处记录的功率之比。计算了地表不同高度丙烷层和不同浓度丙烷层的信息参数值。通过统计建模来量化远程检测丙烷泄漏的有效性。在工作中,计算了丙烷泄漏的正确检测概率(实际发生泄漏时检测到泄漏)和误报警概率(不实际发生泄漏时检测到泄漏)。当信息参数值小于阈值时,决定检测丙烷泄漏。数学建模的结果表明,对于一个丙烷含量至少0.17%的泄漏(一个数量级小于火焰传播的浓度极限),远程检测的问题丙烷泄漏的管道可以解决的正确检测概率超过0.999的假警报的概率小于0.001丙烷层的厚度在地球表面的至少20厘米。
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引用次数: 0
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Telecommunications and Radio Engineering
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