measuring antenna
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Sensors ◽  
2021 ◽  
Vol 21 (12) ◽  
pp. 4005
Author(s):  
Igor Alexandrovich Sidorov ◽  
Alexsandr Grigorevich Gudkov ◽  
Vitalij Yurievich Leushin ◽  
Eugenia Nikolaevna Gorlacheva ◽  
Eugenij Pavlovich Novichikhin ◽  
...  

The possibility of non-invasive determination of the depth of the location and temperature of a cancer tumor in the human body by multi-frequency three-dimensional (3D) radiothermography is considered. The models describing the receiving of the human body’s own radiothermal field processes are presented. The analysis of the possibility of calculating the desired parameters based on the results of measuring antenna temperatures simultaneously in two different frequency ranges is performed. Methods of displaying on the monitor screen the three-dimensional temperature distribution of the subcutaneous layer of the human body, obtained as a result of data processing of a multi-frequency multichannel radiothermograph, are considered. The possibility of more accurate localization of hyperthermia focus caused by the presence of malignant tumors in the depth of the human body with multi-frequency volumetric radiothermography is shown. The results of the study of various methods of data interpolation for displaying the continuous intrinsic radiothermal field of the human body are presented. Examples of displaying the volumetric temperature distribution by the moving plane method based on digital models and the results of an experimental study of the thermal field of the human body and head are given.


Author(s):  
S.D. Kirilyuk

On purpose to increase efficiency of an orbital-frequency resource the usage of polarization-division multiplexing (PDM) is extended in satellite communication systems. For this aim the axis ratio (AR) of polarization ellipses on satellite radio lines with circular (rotating) polarization must be not less 0,94. Nowadays widespread techniques of experimental defining AR, are based on measurements of orthogonal components intensity of electromagnetic fields created by aerials. But, at high, more than 0,85 axis ratios, the information about a difference in components intensity loses on errors of the measurements realizing these techniques. The method of defining AR, close to extremely achievable value (nearly equal to unit) is presented in the article. The basic idea of this method consists in inclusion to the measurement scheme of two identical devices (DUT), working one towards to another. Also the scheme of counter inclusion of two identical DUT, similar used for measurements, may be applied for designing antenna elements with high AR. Good coincidence of results of modeling, laboratory measurements and field tests have confirmed suitability of the offered method for the designing and testing of aerials with high axis ratio.


Author(s):  
A. V. Aksenov

The parametric identification of the mechanism of vertical guidance of the support-rotary device of the measuring antenna complex is carried out. The transfer function is defined, which is presented as a model of the control object. The results of experimental studies allow to determine the average speed of movement of the pivoting device on the corner of the place with the required supply voltage. An integrator and a transfer function of the controller are introduced into the algorithm of the control scheme of the object position. The developed scheme of the control system allows to provide the dynamics corresponding to this speed. The block diagram of the control system implementing the necessary dynamics of the object is given. The control algorithm with the controller is studied using the Matlab 7.9.0 software package. The article presents the logarithmic frequency characteristics of open and closed systems. According to the results of the proposed method of synthesis of the controller for the device, the time of the transient process of the installation is determined; a smooth stop of the device is provided, oscillations are eliminated.


2017 ◽  
Vol 52 (2) ◽  
pp. 27-40
Author(s):  
Karol Dawidowicz ◽  
Radosław Baryła

Abstract Results of long-term static GNSS observation processing adjustment prove that the often assumed “averaging multipath effect due to extended observation periods” does not actually apply. It is instead visible a bias that falsifies the coordinate estimation. The comparisons between the height difference measured with a geometrical precise leveling and the height difference provided by GNSS clearly verify the impact of the near-field multipath effect. The aim of this paper is analysis the near-field interference effect with respect to the coordinate domain. We demonstrate that the way of antennas mounting during observation campaign (distance from nearest antennas) can cause visible changes in pseudo-kinematic precise point positioning results. GNSS measured height differences comparison revealed that bias of up to 3 mm can be noticed in Up component when some object (additional GNSS antenna) was placed in radiating near-field region of measuring antenna. Additionally, for both processing scenario (GPS and GPS/GLONASS) the scattering of results clearly increased when additional antenna crosses radiating near-field region of measuring antenna. It is especially true for big choke ring antennas. In short session (15, 30 min.) the standard deviation was about twice bigger in comparison to scenario without additional antenna. When we used typical surveying antennas (short near-field region radius) the effect is almost invisible. In this case it can be observed the standard deviation increase of about 20%. On the other hand we found that surveying antennas are generally characterized by lower accuracy than choke ring antennas. The standard deviation obtained on point with this type of antenna was bigger in all processing scenarios (in comparison to standard deviation obtained on point with choke ring antenna).


2015 ◽  
Vol 27 (4) ◽  
pp. 43002
Author(s):  
刘敏 Liu Min ◽  
刘小龙 Liu Xiaolong ◽  
晏峰 Yan Feng ◽  
刘瑛 Liu Ying ◽  
熊正锋 Xiong Zhengfeng

Author(s):  
Sergey N. Boyko ◽  
Alexander S. Kukharenko ◽  
Sergey V. Kosiakin ◽  
Dmitry A. Koshevoy ◽  
Yury S. Yaskin

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