ISSUES OF RELIABILITY INSMART ANTENNAS

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Introduction. Adaptive digital antenna arrays, also known as smart antennas, are a perspective direction in the development of ground-based command and meas- urement antenna stations. The basic principles of building of antennas, which are an assembly of analog digital channels with the same center of radiation with a radiation patterns, formed in a digital way, and without phase shift modules, were given a grounding in 1960s [1]. With the progress of electronics, antennas have made a great way from quite simple facilities to complex con- trolled systems with active devices. Interference environment is constantly changing, so that the need in adaptive anten- nas has arisen. Nowadays radio systems are to be able to function under the influence of several heavy broadband interferences in conditions of independent moving of interference sources. In such cases, an adaptive antenna fulfils spatial processing of signal, i. e. it becomes a dy- namic spatial filter. The parallel spatiotemporal signal processing in antenna allows increasing the volume of information received from several satellites simultane- ously. The progress of space technology emphasizes devel- opment of methods of forming stacked beam patterns able to monitor several spacecrafts and to form nulls in direc- tion of interference sources for a ground-based command- measuring complex. The analysis of modern research, methodical and regulatory literature reveals the concern- ment of both state institutions and major space engineer- ing corporation in a substantial upgrade of existing com- mand-measuring complexes characteristics [2]. One of the most prospective ways of development of ground control is using of command-measuring complex equipped with adaptive digital antenna arrays. Such command-measuring complexes would be able, unlike existing stations, to monitor several spacecrafts simultaneously, that will allow increasing the efficiency of data exchange control and performance of technologi- cal operations, reducing control time slot. The development and introduction of smart antennas to ground control systems allow receiving command and telemetric information from all visible satellites. It improves the operational characteristics by elimination of mechanical engineering assemblies of antenna control, and interference immunity of command-measuring comtowards components miniaturization and reducing of their aggregated cost. The nearest future of antenna arrays and especially smart antennas seems to be prospective, while their further development of hardware components will help to solve those problems that suppress mass use of such systems. Reliability of smart antennas is its ability to keep values of technical parameters in set limits in time. It is defined by failures of facilities of smart antennas, mainly, by failures of modules. The requirements to reliability of smart antennas are strict. MTBF is to be at least fifty thousand hours, while assured life should be not less than 10 years. Faultiness of electronic components in the modules determine the appearance of both sudden failures and gradual failures. The first lead to the fact that the emitters of smart antennas connected to the failed modules have a zero amplitude of excitation, the second causes a change in the complex amplitudes of the excitation emitters. Since smart antenna is a statistical system, which includes a large number of parallel channels, it potentially has high reliability. Indeed, both types of failures of the modules lead not to failure of the whole system, but only to a dete- rioration of energy and the directivity characteristics of the antenna: reducing the effective area, increasing the error of the beam, increasing the level of side lobes, reducing the transmission power of the transmitting smart antenna [7-9]. The failure rate of the modules l(t) is a function of time. With good accuracy we can assume that after screening tests the failure rate of the modules is constant, i. e. l(t) = l = const. The percentage of modules failed for the time t, is given by the following ratio: plex due to spatial-temporal processing of signals. n(t) / N = 1- exp(-l t), (1) The advantages of digital antenna arrays are [3-5]: - presenting digital synthesis of a radiation pattern in a receiving mode and forming of specified distribution of electromagnetic field in an antenna array face in transmit- ting mode; - the ability of digital antenna arrays to perform mul- tisignal transmit and receive signals in a spatial angle; - the ability to perceive all the information contained in the structure of spatial-temporal electromagnetic fields in an antenna array face and transform it into data almost without any losses; where n(t) is the quantity of failed modules; N is the total quantity of modules, T0 = l-1 is MTBF. n(t) / N » l t = t /T0 is true for t << T0. The value T0 of the electronic components of the elec- tronic equipment specified in the specifications. The failure rate of the modules essentially depends on the operating temperature of the crystals of semiconductor devices included in the modules. Description of tempera- ture dependence of MTBF is based on the Arrhenius equation: - the digital formation of the requested radiation patl(T ) = A exp(-e / kT ), (2) tern in receivers input provides deep spatial cancellation. When combined with the volume expansion it provides interference immunity unreachable before. Smart antennas allow implementing of special types of gain-phase distribution in an antenna array face and applying for different methods of processing of signals received by every single antenna radiating element. Therefore, it is possible to gain low side lobes of the radiation pattern, to extract more data out of the received from different satellites radio waves, to use adaptive algo- rithms of optimal spatial-temporal filtration of signals against a background of interference, that all in all improves characteristics of navigational facilities of a consumer [6]. Modern hardware components allow producing smart antennas with unique specifications along with the trend where T is the absolute temperature; k is the Boltzmann’s constant; e is activation energy; A is the constant of pro- portionality. Test results show that at temperatures of the crystal of 100-200 °C, the failure rate increases about 2 times by increasing the working temperature to 10 °C. That is, when the temperature increases, for example, from 100 to 150 °C operating time to failure is reduced by more than 30 times. In this regard, when considering reli- ability issues, the first thing to pay attention are transmit- ting adaptive digital antenna arrays having elevated oper- ating temperature due to large heat generation and there- fore lower reliability [10]. From the above it follows that a major problem in the design of transmitting adaptive digital antenna arrays is to ensure the normal thermal regimes of high-power transis- tors with the purpose of increasing their reliability. If dissipation is large, a liquid cooling system is used, at relatively low heat an air cooling system is applied. Cooling systems working on different physical principles may be used as well. Here is the example of reliability The average error of the maximum of a radiation pat- tern dq related to the width of the half power radiation pattern Dq05 (for the case of square pattern) is given by: calculations for smart antennas. dq / Dq05 » 0.3 a / N . (5) Adaptive digital antenna arrays with large heat genera- tion use liquid cooling systems. Some smart antennas are made of tile-typed modules with metal thermal busses, The distribution of the side lobes of the radiation pat- tern obeys the generalized Rayleigh law. Average level of side lobes is described by the ratio: б б0 in which heat from the power transistors is transmitted to the piping with the coolant fluid, located on the rear side f 2 = f 2 + a p / N , (6) of smart antenna. In order to remove high heat generation module structures with embedded channels for flushing of where 2 is the relative significance of any side lobe of f б0 cooling liquid are used. For smart antenna of K-range communication system (18.8-19.3 GHz) RaytheonSystemsCompany designed a cooling system, based on using phase transitions of the refrigerant. The heat exchanger in the form of a metal cylinder filled with porous aluminum “foam”, impreg- f б power in the absence of amplitude-phase errors; 2 is the average value of the same side lobe if there are errors. In a separate implementation level of the side lobe can be more. With a probability almost equal to one, the maxi- mum level of lateral radiation does not exceed values: nated with paraffin wax. The volume of the heat exchanger and modules are connected by heat pipes. f1 = fб0 + 3 a p / 2N . (6a) When you enable the modules the heat supplied to the heat exchanger volume goes into melting the paraffin. In 80 % of implementations, the level of the side lobe does not exceed the value The process occurs at almost constant temperature. After turning off the modules, the process is reversed - the parf2 = fб0 + a p / 2N . (6b) affin sets solid. The heat exchange device provides the junction temperature of the transistors about 100 °C when temperature gradients on the surface of the array is less than 10 °C. Changes in the characteristics of smart antennas due to failures of modules can be described by statistical meth- ods. An average radiation pattern of power of a system consisting of N emitters has the form: 2 r r F (k , k0 ) = To assess the level of first side lobe of a smart antenna with a square aperture under equiamplitude excitation of the emitters in the formulas (6) should be considered fб0 = 0.217. The degradation of the gain depends only on a, and the side radiation caused by random errors, decreases with increasing N. Thus, the maximum level of the first side lobe (6a) of the array with a rectangular aperture that is 13.2 dB with no errors (a = 0) is increased in the presence of the error a = 0.3 to -8.8 dB in the array with N = 200, N r r r 2 (3) and only up to 12.7 dB in the array with N = 20000. = å In (1+ An ) ei (k - k0 , rn ) ei Fn , n=1 r For the same parameters relative error of the maximum radiation pattern (5) is approximately 1 % of the beam width at N = 200 and only 0.1 % when N = 20000. where k is the wave vector directed towards the observar The ratio (4)-(6) can be used to assess the impact tion point; k0 is the wave vector directed towards the of the modules breakdown on the performance of smart system phasing point; r f (k ) 2 is an average radiation patantennas. In the statistical theory of antenna arrays it is shown tern of power; r rn is the vector assigning location of emitthat the failure of n randomly located in the array of N elements can be considered equivalent to the impact ter nth; In is the deterministic part of the amplitude excitation of the nth radiator; Аn, Фn - random amplitude and phase errors of the excitation of the nth emitter. The rela- tion (3) allows by averaging the ensemble of realizations of the random radiation patterns of smart antennas to find of uniformly distributed over all elements of the array of random amplitude and phase errors with variance a = n/N. Expressing the fraction of the failed elements as a function of the failure rate (1), we get: a = a (t) = n(t) / N = the dependence of its parameters from the parameters of a random amplitude-phase errors [11; 12]. = 1 - e-lt » l t = t / T0 . (7) If the amplitude and phase errors in the channels are independent and small, i. e. they have a zero average and small variance a = ( A2 + F2 ) << 1 , and average values n n of the amplitudes are the same ( In = 1), then degradation of smart antennas parameters is described by the following approximate relations. The gain is determined by the ratio: It should be borne in mind that the failure of modules of the transmitting adaptive digital antenna arrays not only leads to deterioration of the gain and radiation pattern, but will also reduce the radiated power, so the potential of smart antennas when n << N is described by the following ratio: П = PG = П0 (1 - a)e-a » G = G 0 - DG » G0 e-a » G0 (1 - a ). (4) » П0 (1 - a)2 = П0 (1 - t / T0 )2. (8) Авиационная и ракетно-космическая техника Time to failure Т0 of modern transistor transceiving modules of smart antennas of X-range is up to 100 000 hours (over 11 years). Receiver modules, made by hybrid tech- nology have a life 2-3 times longer, and receiver modules based on integrated circuit can take Т0 > 1 000 000 hours, that is orders of magnitude larger. From ratios (7)-(8) it follows that the smart antenna with N = 20 000 modules and T0 = 100 000 hours, will undergo the following changes of parameters after one year operation without repair (about 8600 hours): decrease of the gain and effective area of the aperture (about 0.4 dB), the reduction of potential (about 0.8 dB), maximum growth of the first side lobe (not more than 0.3 dB), the maximum error of the beam (about 0.2 %, without taking into account the error, associated with the discrete- ness of the phase shifters and errors in the calibration of the channels of the array). Given parameters are achievable, if the correct ther- mal operation mode of power transistors is chosen. This is achieved through the optimal mode of operation at a re- duced power level, rational choice of materials for body- work and its design maximizing heat dissipation from the crystals, a sufficient flow of cooling air or fluid in the cooling system [13-15]. Practically, the modules located at the edges of the ap- erture have a lower temperature than the modules located in the central part due to heat transfer to the environment. For example, in the literature there are the results of tests of a 17-element active array with air cooling. Power con- sumption of DC power in each channel is 9 watts. In con- ditions of the absence of forced cooling central elements of the array have a temperature of about 100 °С while the extreme ones - 60 °С. When enabled forced airflow, those temperatures are 40 °С and 20 °С, respectively [16]. Increased temperature in the central part of the aper- ture leads to a higher failure rate of the modules located here in accordance with the aforementioned ratio (2). This, in turn, leads to higher growth of side radiation than it follows from (6). Simulation of smart antennas parame- ters with variable temperature distribution can be per- formed using the ratio (3), while the failure rate of the modules in the aperture is described by the ratio (2). Conclusion. Thus, for a more accurate description of the smart antennas characteristics it is necessary to create a model of its reliability. Such a model should take into account energy parameters of the modules and their ele- ments, the dependence of the efficiency (and hence oper- ating temperature) from the output power level, the tem- perature dependence on structural parameters of the cool- ing system, the above mentioned dependence of MTBF on the temperature, a more accurate description of the failure rate of the modules based on the analysis of the failure rate of their elements.

Sobre autores

I. Kartsan

Reshetnev Siberian State University of Science and Technology

Email: kartsan2003@mail.ru
31, Krasnoyarsky Rabochy Av., Krasnoyarsk, 660037, Russian Federation

E. Kiseleva

22 NIO 2 NIU NIC VA Peter the Great

8, Karbysheva Str., Balashikha, Moscow region, 143900, Russian Federation

L. Skopintseva

22 NIO 2 NIU NIC VA Peter the Great

8, Karbysheva Str., Balashikha, Moscow region, 143900, Russian Federation

E. Shangina

JSC “Academician M. F. Reshetnev Information Satellite Systems”

52, Lenin Street, Zheleznogorsk, Krasnoyarsk region, 662972, Russian Federation

S. Efremova

Reshetnev Siberian State University of Science and Technology

31, Krasnoyarsky Rabochy Av., Krasnoyarsk, 660037, Russian Federation

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