scholarly journals Automatic Algorithm for Extracting the Jet Engine Information from Radar Target Signatures of Aircraft Targets

Author(s):  
Woo-Yong Yang ◽  
Ji-Hoon Park ◽  
Jun-Woo Bae ◽  
Seong-Cheol Kang ◽  
Chan-Hong Kim ◽  
...  
2015 ◽  
Vol 30 (7) ◽  
pp. 18-29 ◽  
Author(s):  
Woo Yong Yang ◽  
Ji Hoon Park ◽  
Jun Woo Bae ◽  
Noh Hoon Myung ◽  
Chan Hong Kim

2021 ◽  
Vol 21 (5) ◽  
pp. 417-424
Author(s):  
Woo-Yong Yang ◽  
Dal-Jae Yun ◽  
Dong-Wook Seo

One of the major issues in multifunction radars is time resource allocation to maximize the radar’s ability. If jet engine modulation (JEM) is more efficiently performed in an insufficient dwell-time environment, the remaining time can be allocated for other tasks. This study presents a novel automatic algorithm for estimating the jet engine blade number of insufficient JEM signals. We employed a harmonic selection rule and a modified empirical mode decomposition (EMD) with an adaptive low-pass filtering. For a refined autocorrelation waveform, the analysis focuses on a desirable combination of intrinsic mode functions derived from the modified EMD. The approach is significant because it enables reliable estimation despite the insufficient JEM signal. Also, the proposed algorithm is innovative because it uses only the time-domain method, not the frequency-domain method. The application is expected to enhance the efficiency of radar resource management.


2014 ◽  
Vol 28 (8) ◽  
pp. 963-975 ◽  
Author(s):  
Ji-Hoon Park ◽  
Woo-Yong Yang ◽  
Jun-Woo Bae ◽  
Seong-Cheol Kang ◽  
Chan-Hong Kim ◽  
...  

2017 ◽  
Vol 17 ◽  
pp. 245-252
Author(s):  
V. V. Somov

In carrying out an investigation into the explosion, among others, the investigative version of the use of a single-use reactive grenade launcher is being considered. The most common for criminal explosions are applied grenade launchers RPG-18, RPG-22, RPG-26. Their use is due to a number of such properties as small size and weight, which makes it possible to transfer them covertly, the range of the shot significantly exceeding the range of the hand grenade throw, the high detonating effect of the rocket grenade explosion. The single-use rocket launchers are generally of the same design. Their differences are in the features of the components construction and dimensional characteristics, which are given in the article. On the basis of expert practice, details ofgrenade launchers that remain at the site of the explosion and have the least damage are determined. These details are the objects of investigation of the explosion technical expertise. These objects include launchers of grenade launchers and rocket parts ofjet grenades. The design features of the launchers, their dimensional characteristics and marking symbols make it possible to determine their belonging to a specific type of jet grenade launchers. Missile parts of jet grenades differ in the form of the combustion chamber of the jet engine, nozzle, in the size ofthe outlet section of the nozzle, in the form and size of the stabilizerfeathers. To determine the belonging of the rocket part of the grenade to a specific type ofjet grenade launcher, it’s necessary to establish a set of structural features and dimensional characteristics. At considerable damage of the combustion chamber of the jet engine, as a rule, the nozzle block remains intact that allows to define diameter of critical section of a nozzle, and on it to establish type of the used single-use grenade launcher.


2000 ◽  
Author(s):  
A. Armendariz ◽  
D. Leith ◽  
M. Boundy ◽  
R. Goodman ◽  
L. Smith

2017 ◽  
Vol 25 (101) ◽  
pp. 74-75
Author(s):  
Alexey Viktorovich Kachura ◽  
◽  
Sergej V., Kolychev ◽  
Alexander Mikhailovich, Syanov
Keyword(s):  

Author(s):  
Devdas Shetty ◽  
Tom Eppes ◽  
Nikolay Nazaryan ◽  
Claudio Campana ◽  
Jun Kondo

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