Detection Small Aircraft by Acoustic Radiation

被引:6
作者
Kozeruk, S. O.
Korzhyk, O., V
机构
来源
VISNYK NTUU KPI SERIIA-RADIOTEKHNIKA RADIOAPARATOBUDUVANNIA | 2019年 / 76期
关键词
small aircraft; typical detection channel; detection characteristics; maximum detection range;
D O I
10.20535/RADAP.2019.76.15-20
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
Introduction. The problem of detecting small aircraft (SA) gave impetus to the creation of devices and systems for detecting different principles of operation. The detection of drones is complicated by their low visibility, both in the electromagnetic and acoustic ranges of the wavelengths and the feature of the flight path. Flight altitude can vary from units to tens of meters, and the dynamics of movement, from lagging to acceleration in an arbitrary direction. The use of radar allows detect drones in open areas at a distance of up to 1000m. Acoustic observation methods provide detection in complex terrain and the presence of green spaces. The detection range depends on the selected receiver, the radiation level of the object and the level of acoustic noise in the observation area. The development of the algorithm for calculating the detection range for the given detection characteristics seems to be relevant. Theoretical results. For the detection of flying objects it is proposed to use a receiver that provides non-coherent processing of acoustic signals - typical detection channel. The algorithm for calculating the maximum range of detection of SA is based on the statistical theory of detecting a noise-like signal disguised by interference. The algorithm for calculating the maximum detection range of SA is based on the statistical theory of detection of a noise-like signal. The sequence of calculating the maximum range of detection of LLA is reduced to establishing the type, effective frequency band and level of the radiation signal, determining the level of interference in the reception area, calculating the CW detection parameter, calculating the maximum detection range. Conclusions. To detect SA by acoustic radiation, it is proposed to use a detector according to the scheme of a typical detection channel. An algorithm for calculating the probability of detecting a noise signal is presented and a decision rule is established. The paper proposes an algorithm for calculating the maximum distance for detection of SA. An important factor in assessing the range is the distribution of air temperature with altitude and the direction of movement of air masses. Therefore, the algorithm should be improved taking into account the meteorological situation.
引用
收藏
页码:15 / 20
页数:6
相关论文
共 16 条
[11]   Development and test of a low-cost 3D-Display for small aircraft [J].
Sachs, G ;
Sperl, R ;
Nothnagel, K .
ENHANCED AND SYNTHETIC VISION 2002, 2002, 4713 :160-167
[12]   A Diesel Engine with a Catalytic Piston Surface to Propel Small Aircraft at High Altitudes-A Theoretical Study [J].
Karsenty, Kadmiel ;
Tartakovsky, Leonid ;
Sher, Eran .
ENERGIES, 2021, 14 (07)
[13]   Correction of the Model for Assessing the Emission of Harmful Exhaust Emissions from the Engine of a Small Aircraft During the Flight [J].
Markowski, Jaroslaw .
INAIR 2018: AVIATION ON THE GROWTH PATH, 2018, 35 :230-239
[14]   Overview of Detection and Localization Methods of Small Unmanned Aerial Vehicles [J].
Sokolskyi, S. O. ;
Movchanyuk, A. V. .
VISNYK NTUU KPI SERIIA-RADIOTEKHNIKA RADIOAPARATOBUDUVANNIA, 2021, (87) :46-55
[15]   Proposal of an automatic Flight Time measurement method for small aircraft using a built-in smartphone 3-axis accelerometer [J].
Kawai S. ;
Wada T. ;
Ebara H. .
IEEJ Transactions on Electronics, Information and Systems, 2021, 141 (06) :743-751
[16]   Temperature-compensated strain measurement of full-scale small aircraft wing structure using low-cost FBG interrogator [J].
Kim, J. H. ;
Lee, Y. G. ;
Park, Y. ;
Kim, C. G. .
SENSORS AND SMART STRUCTURES TECHNOLOGIES FOR CIVIL, MECHANICAL, AND AEROSPACE SYSTEMS 2013, 2013, 8692