Íàöèîíàëüíûé àýðîêîñìè÷åñêèé óíèâåðñèòåò èì. Í.Å. Æóêîâñêîãî “Õàðüêîâñêèé àâèàöèîííûé èíñòèòóò”

 

 

ISSN 1727-7337. À²ÀÖ²ÉÍÎ-ÊÎÑ̲×ÍÀ ÒÅÕͲÊÀ  ² ÒÅÕÍÎËÎòß. – 2013. – ¹ 10(107). – 260 ñ.

ISSN 1727-7337. ÀÂÈÀÖÈÎÍÍÎ-ÊÎÑÌÈ×ÅÑÊÀß ÒÅÕÍÈÊÀ È ÒÅÕÍÎËÎÃÈß. – 2013. – ¹ 10(107). – 260 ñ.

ISSN 1727-7337. AEROSPACE TECHNIC AND TECHNOLOGY. – 2013. – ¹ 10(107). – 260 ñ.

 

ÑÒÀÒÜè (articleS)

 

Àâòîðû
(ÿçûê
îðèãèíàëà)

Íàçâàíèå ñòàòüè  (article title)

Ñòðàíèöû

(pages)

English

Óêðà¿íñüêà ìîâà

Ðóññêèé ÿçûê

Òåõíîëîãèÿ ïðîèçâîäñòâà ëåòàòåëüíûõ àïïàðàòîâ

Êîìáàðîâ Â.Â.,
Ñîðîêèí Â.Ô.

THE PROVIDING STABILITY OF CONTOUR FEEDRATE IN CNC SYSTEM BY HIGH-SPEED EQUIPMENT ON EXAMPLE OF CIRCULAR INTERPOLATION

ÇÀÁÅÇÏÅ×ÅÍÍß ÑÒÀÁIËÜÍÎÑÒI ÊÎÍÒÓÐÍί ÏÎÄÀ×I  ÑÈÑÒÅ̲ ×ÏÓ ÂÈÑÎÊÎØÂÈÄÊIÑÍÎÃÎ ÎÁËÀÄÍÀÍÍß ÍÀ ÏÐÈÊËÀIJ ÊÐÓÃÎÂί IÍÒÅÐÏÎËßÖI¯

ÎÁÅÑÏÅ×ÅÍÈÅ ÑÒÀÁÈËÜÍÎÑÒÈ ÊÎÍÒÓÐÍÎÉ ÏÎÄÀ×È Â ÑÈÑÒÅÌÅ ×ÏÓ ÂÛÑÎÊÎÑÊÎÐÎÑÒÍÛÌ ÎÁÎÐÓÄÎÂÀÍÈÅÌ ÍÀ ÏÐÈÌÅÐÅ ÊÐÓÃÎÂÎÉ ÈÍÒÅÐÏÎËßÖÈÈ

7–14
(8)

Íåâåøêèí Þ.À.,
×åõðåñàç Ì.,
Òðåòüÿê Â.Â.,
Îíîï÷åíêî À.Â.

OPTIMIZATION TECHNOLOGY MANUFACTURING DETAIL TYPE COUPLING HALF USING A SOFTWARE PACKAGE DEFORM

ÎÏÒÈ̲ÇÀÖ²ß ÒÅÕÍÎËÎò¯ ÂÈÃÎÒÎÂËÅÍÍß ÄÅÒÀ˲ ÒÈÏÓ ÏÎËÓÌÓÔÒÀ Ç ÂÈÊÎÐÈÑÒÀÍÍßÌ ÏÐÎÃÐÀÌÍÎÃÎ ÏÀÊÅÒÓ DEFORM

ÎÏÒÈÌÈÇÀÖÈß ÒÅÕÍÎËÎÃÈÈ ÈÇÃÎÒÎÂËÅÍÈß ÄÅÒÀËÈ ÒÈÏÀ ÏÎËÓÌÓÔÒÀ Ñ ÈÑÏÎËÜÇÎÂÀÍÈÅÌ ÏÐÎÃÐÀÌÌÍÎÃÎ ÏÀÊÅÒÀ DEFORM

15–19
(5)

Óìàíñêèé À.Ï.,
Ïîëÿðóñ Å.Í.,
Óêðàèíåö Ì.Ñ.,
Äîâãàëü À.Ã.,
Êàïèòàí÷óê Ë.Ì.,
Ñóááîòèí Â.È.

THE STRUCTURE AND PROPERTIES INVESTIGATIONS OF COMPOSITE MATERIALS AND COATINGS BASED ON NiAl-TiB2 SYSTEMS

ÄÎÑË²ÄÆÅÍÍß ÑÒÐÓÊÒÓÐÈ ÒÀ ÂËÀÑÒÈÂÎÑÒÅÉ ÊÎÌÏÎÇÈÖ²ÉÍÈÕ ÌÀÒÅвÀ˲ ÒÀ ÏÎÊÐÈÒÒ²Â Ç ÍÈÕ ÍÀ ÎÑÍβ ÑÈÑÒÅÌÈ NiAl-TiB2

ÈÑÑËÅÄÎÂÀÍÈÅ ÑÒÐÓÊÒÓÐÛ È ÑÂÎÉÑÒÂ ÊÎÌÏÎÇÈÖÈÎÍÍÛÕ ÌÀÒÅÐÈÀËÎÂ È ÏÎÊÐÛÒÈÉ ÈÇ ÍÈÕ ÍÀ ÎÑÍÎÂÅ ÑÈÑÒÅÌÛ NiAl-TiB2

20–24
(5)

Ïðîåêòèðîâàíèå àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ àïïàðàòîâ

Íèêîëàåâ Â.Í.,
Êàáàíîâ Þ.Í.

A THERMAL-CONVECTION TRANSDUCER OF FLUID CONSUMPTION AND TEMPERATURE IN PIPELINES OF AIRCRAFT ENGINE

ÒÅÐÌÎÊÎÍÂÅÊÒÈÂÍÈÉ ÏÅÐÅÒÂÎÐÞÂÀ× ÂÈÒÐÀÒÈ ² ÒÅÌÏÅÐÀÒÓÐÈ Ð²ÄÈÍÈ Â ÒÐÓÁÎÏÐÎÂÎÄÀÕ ÄÂÈÃÓÍÀ ˲ÒÀËÜÍÎÃÎ ÀÏÀÐÀÒÀ

ÒÅÐÌÎÊÎÍÂÅÊÒÈÂÍÛÉ ÏÐÅÎÁÐÀÇÎÂÀÒÅËÜ ÐÀÑÕÎÄÀ È ÒÅÌÏÅÐÀÒÓÐÛ ÆÈÄÊÎÑÒÈ Â ÒÐÓÁÎÏÐÎÂÎÄÀÕ ÄÂÈÃÀÒÅËß ËÅÒÀÒÅËÜÍÎÃÎ ÀÏÏÀÐÀÒÀ

25–29
(5)

Èãóìåíöåâ Å.À.,
Ïðîêîïåíêî Å.À.

ELECTROMAGNETIC COMPONENTS OF THE CHARGED GYROSCOPE rotational frequency

Åëåêòðîìàãí³òí³ ñêëàäîâ³ ÷àñòîòè îáåðòàííÿ çàðÿäæåíîãî  ã³ðîñêîïó

ÝËÅÊÒÐÎÌÀÃÍÈÒÍÛÅ ÑÎÑÒÀÂËßÞÙÈÅ ×ÀÑÒÎÒÛ ÂÐÀÙÅÍÈß ÇÀÐ߯ÅÍÍÎÃÎ ÃÈÐÎÑÊÎÏÀ

30–36
(7)

Äâèãàòåëè è ýíåðãîóñòàíîâêè àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ àïïàðàòîâ

Êèðè÷êîâ Ì.À.,
Åëàíñêèé À.Â.,
Êðàâ÷åíêî È.Ô.

DEVELOPING A SMALL-SIZE FAMILY OF GAS TURBINE ENGINE BASED ON SINGLE CORE

ÑÒÂÎÐÅÍÍß Ñ²ÌÅÉÑÒÂÀ ÌÀËÎÐÎÇ̲ÐÍÈÕ ÃÀÇÎÒÓÐÁ²ÍÍÈÕ ÄÂÈÃÓͲ ÍÀ ÁÀDz ªÄÈÍÎÃÎ ÃÀÇÎÃÅÍÅÐÀÒÎÐÀ

ÑÎÇÄÀÍÈÅ ÑÅÌÅÉÑÒÂÀ ÌÀËÎÐÀÇÌÅÐÍÛÕ ÃÀÇÎÒÓÐÁÈÍÍÛÕ ÄÂÈÃÀÒÅËÅÉ ÍÀ ÁÀÇÅ ÅÄÈÍÎÃÎ ÃÀÇÎÃÅÍÅÐÀÒÎÐÀ

37–41
(5)

Ëîÿí À.Â.,
Êîøåëåâ Í.Í.,
Öàãëîâ À.È.,
Òèòîâ Ì.Þ.

INVESTIGATION OF THERMAL FLUXES DISTRIBUTION IN THE CONSTRUCTION OF HEATERLESS HOLLOW CATHODE FOR ELECTRIC PROPULSION IN OPERATING CURRENT RANGE UP TO 50 A

ÄÎÑË²ÄÆÅÍÍß ÐÎÇÏÎIJËÓ ÒÅÏËÎÂÈÕ ÏÎÒÎÊ²Â Ó ÊÎÍÑÒÐÓÊÖ²¯ ÁÅÇÍÀÊÀËÜÍÎÃÎ ÏÎËÎÃÎ ÊÀÒÎÄÓ ÅÐÄ ÏÐÈ ÐÎÁÎ×ÈÕ ÑÒÐÓÌÀÕ ÄÎ 50 À

ÈÑÑËÅÄÎÂÀÍÈÅ ÐÀÑÏÐÅÄÅËÅÍÈß ÒÅÏËÎÂÛÕ ÏÎÒÎÊΠ ÊÎÍÑÒÐÓÊÖÈÈ ÁÅÇÍÀÊÀËÜÍÎÃÎ ÏÎËÎÃÎ ÊÀÒÎÄÀ ÝÐÄ  ÏÐÈ ÐÀÁÎ×ÈÕ ÒÎÊÀÕ ÄÎ 50 À

42–46
(5)

Âèíîãðàäîâ À.Ñ.,
Áàäûêîâ Ð.Ð.,
Ìèðîíîâ À.Â.

CREATING OF METHOD FOR SUPPORT SEAL AIRCRAFT ENGINE DESIGN WITH THE PARAMETERS OF OIL SYSTEM

ÐÎÇÐÎÁÊÀ ÌÅÒÎÄÈÊÈ ÏÐÎÅÊÒÓÂÀÍÍß ÓÙ²ËÜÍÅÍÍß ÎÏÎÐÈ À²ÀÖ²ÉÍÈÕ ÄÂÈÃÓÍ²Â Ç ÓÐÀÕÓÂÀÍÍßÌ ÏÀÐÀÌÅÒв ÌÀÑËßÍί ÑÈÑÒÅÌÈ

ÐÀÇÐÀÁÎÒÊÀ ÌÅÒÎÄÈÊÈ ÏÐÎÅÊÒÈÐÎÂÀÍÈß ÓÏËÎÒÍÅÍÈß ÎÏÎÐÛ ÀÂÈÀÖÈÎÍÍÎÃÎ ÄÂÈÃÀÒÅËß Ñ Ó×ÅÒÎÌ ÏÀÐÀÌÅÒÐΠÌÀÑËßÍÎÉ ÑÈÑÒÅÌÛ

47–50
(4)

Íîâèêîâ Ä.Ê.,
Åðìîëàåâ Ã.Ì.

MODELLING OF THE SQUEEZED FILM DAMPER IN A FLUENT

Ìîäåëþâàííÿ ã³äðîäèíàì³÷íîãî äåìïôåðà â ïàêåò³ Fluent

ÌÎÄÅËÈÐÎÂÀÍÈÅ ÃÈÄÐÎÄÈÍÀÌÈ×ÅÑÊÎÃÎ ÄÅÌÏÔÅÐÀ  ÏÀÊÅÒÅ FLUENT

51–54
(4)

Âîðîáüåâ Þ.Ñ.,
Ðîìàíåíêî Â.Í.,
Òûðòûøíèêîâ Ê.Ä.,
Êóëèøîâ Ñ.Á.,
Ñêðèöêèé À.Í.

Analysis of vibrations of gas turbine compressor blading

Àíàë³ç êîëèâàíü ëîïàòêîâîãî àïàðàòó êîìïðåñîðà ÃÒÄ

ÀÍÀËÈÇ ÊÎËÅÁÀÍÈÉ ËÎÏÀÒÎ×ÍÎÃÎ ÀÏÏÀÐÀÒÀ ÊÎÌÏÐÅÑÑÎÐÀ ÃÒÄ

55–59
(5)

Íàçàðåíêî Þ.Á.

AVOIDANCE OF RESONANCE WITH ROTOR'S CRITICAL REVOLUTION FREQUENCY IN CASE OF ELLIPTIC TRAJECTORY OF BEARING SHAFT AXIS REVOLUTION ON SUPPORT BEARING

ÓÑÓÍÅÍÍß ÐÅÇÎÍÀÍÑÓ ÍÀ ÊÐÈÒÈ×ÍIÉ ×ÀÑÒÎÒI ÎÁÅÐÒÀÍÍß ÐÎÒÎÐI ÏÐÈ EËIÏÒÈ×ÍIÉ ÒÐÀªÊÒÎÐI¯ ÎÁÅÐÒÀÍÍß ÂIÑI ÂÀËÓ ÍÀ ÎÏÎÐI

ÓCÒÐÀÍÅÍÈÅ ÐÅÇÎÍÀÍÑÀ ÍÀ ÊÐÈÒÈ×ÅÑÊÎÉ ×ÀÑÒÎÒÅ ÂÐÀÙÅÍÈß ÐÎÒÎÐΠÏÐÈ ÝËËÈÏÒÈ×ÅÑÊÎÉ ÒÐÀÅÊÒÎÐÈÈ ÂÐÀÙÅÍÈß ÎÑÈ ÂÀËÀ ÍÀ ÎÏÎÐÅ

60–65
(6)

Ôåäîð÷åíêî Ä.Ã.,
Ãëàäêîâ À.Â.,
Ñîëÿííèêîâ Â.À.,
Æóæóêèí À.È.

THE USE OF HOLOGRAPHIC INTERFEROMETRY FOR ROTATING OBJECT VIBRATIONS STUDY

ÇÀÑÒÎÑÓÂÀÍÍß ÃÎËÎÃÐÀÔ²×Íί ²ÍÒÅÐÔÅÐÎÌÅÒв¯ ÄËß ÄÎÑË²ÄÆÅÍÍß ÊÎËÈÂÀÍÜ ÎÁ’ªÊÒ²Â, ÙÎ ÎÁÅÐÒÀÞÒÜÑß

ÏÐÈÌÅÍÅÍÈÅ ÃÎËÎÃÐÀÔÈ×ÅÑÊÎÉ ÈÍÒÅÐÔÅÐÎÌÅÒÐÈÈ ÄËß ÈÑÑËÅÄÎÂÀÍÈß ÊÎËÅÁÀÍÈÉ ÂÐÀÙÀÞÙÈÕÑß ÎÁÚÅÊÒÎÂ

66–71
(6)

Êóëèêîâ Ã.Ã.,
Àáäóëíàãèìîâ À.È.,
Áàäàìøèí Á.È.,
×åïàéêèí À.Ñ.

CALCULATION OF SMALL PARAMETERS IN PROPELLERS CONTROL SYSTEM MODEL OF TURBOFAN ENGINES

ÓÐÀÕÓÂÀÍÍß ÌÀËÈÕ ÏÀÐÀÌÅÒв ÌÎÄÅ˲ ÑÈÑÒÅÌÈ ÓÏÐÀÂ˲ÍÍß ÃÂÈÍÒÎÂÅÍÒÈËßÒÎÐÀ ÒÃÂÄ

Ó×ÅÒ ÌÀËÛÕ ÏÀÐÀÌÅÒÐΠÌÎÄÅËÈ ÑÈÑÒÅÌÛ ÓÏÐÀÂËÅÍÈß ÂÈÍÒÎÂÅÍÒÈËßÒÎÐÀ ÒÂÂÄ

72–81
(10)

Åïèôàíîâ Ñ.Â.,
Êîíîíûõèí Å.À.

SYNTHESIS AND ANALYSIS OF AN ADVANCED GAS TURBINE ENGINE CONTROL

ÑÈÍÒÅÇ ² ÀÍÀË²Ç ÏÅÐÑÏÅÊÒÈÂÍί ÑÀÓ ÃÒÄ

ÑÈÍÒÅÇ È ÀÍÀËÈÇ ÏÅÐÑÏÅÊÒÈÂÍÎÉ ÑÀÓ ÃÒÄ

82–86
(5)

Ïàí³í Â.Â.,
ªí÷åâ Ñ.Â.,
Ñàâ÷èí Î.Â.

ALGORITHMIC MAINTENANCE OF A SYSTEM OF IDENTIFICATION PRESURGE (OF SURGE) PHENOMENA IN COMPRESSORS AVIATION GTE

ÀËÃÎÐÈÒ̲×ÍÅ ÇÀÁÅÇÏÅ×ÅÍÍß ÔÓÍÊÖ²ÎÍÓÂÀÍÍß ÑÈÑÒÅÌÈ ²ÄÅÍÒÈÔ²ÊÀÖ²¯ ÏÅÐÅÄÏÎÌÏÀÆÍÈÕ (ÏÎÌÏÀÆÍÈÕ) ßÂÈÙ Ó ÊÎÌÏÐÅÑÎÐÀÕ À²ÀÖ²ÉÍÈÕ ÃÒÄ

ÀËÃÎÐÈÒÌÈ×ÅÑÊÎÅ ÎÁÅÑÏÅ×ÅÍÈÅ ÔÓÍÊÖÈÎÍÈÐÎÂÀÍÈß ÑÈÑÒÅÌÛ ÈÄÅÍÒÈÔÈÊÀÖÈÈ ÏÐÅÄÏÎÌÏÀÆÍÛÕ (ÏÎÌÏÀÆÍÛÕ) ßÂËÅÍÈÉ Â ÊÎÌÏÐÅÑÑÎÐÀÕ ÀÂÈÀÖÈÎÍÍÛÕ ÃÒÄ

87–91
(5)

Bradac M.,
Zouhar F.,
Krizan J.,
Bliznak M.,
Vargovcik L.,
Kononikhyn O.,
Pavlyuk Y.,
Kravchenko Y.

MODEL BASED DESIGN APPLIED FOR DEVELOPMENT OF FUEL METERING PUMP CONTROL ALGORITHM

ÇÀÑÒÎÑÓÂÀÍÍß ÌÎÄÅËÜÍÎ-ÎвªÍÒÎÂÀÍÎÃÎ ÏÐÎÅÊÒÓÂÀÍÍß ÄËß ÐÎÇÐÎÁÊÈ ÀËÃÎÐÈÒÌÓ ÓÏÐÀÂ˲ÍÍß ÍÀÑÎÑÎÌ-ÄÎÇÀÒÎÐÎÌ

ÏÐÈÌÅÍÅÍÈÅ ÌÎÄÅËÜÍÎ-ÎÐÈÅÍÒÈÐÎÂÀÍÍÎÃÎ ÏÐÎÅÊÒÈÐÎÂÀÍÈß ÄËß ÐÀÇÐÀÁÎÒÊÈ ÀËÃÎÐÈÒÌÀ ÓÏÐÀÂËÅÍÈß ÍÀÑÎÑÎÌ-ÄÎÇÀÒÎÐÎÌ

92–96
(5)

Ïàâëþê Å.Â.,
Êðàâ÷åíêî Þ.È.,
Åïèôàíîâ Ñ.Â.,
Ñóõîâåé Ñ.È.

APPLICATION OF THE STEPPER DRIVE IN THE FUEL METERING SYSTEMS DEVELOPED BY SE “KhADB

ÇÀÑÒÎÑÓÂÀÍÍß ÊÐÎÊÎÂÎÃÎ ÅËÅÊÒÐÎÏÐÈÂÎÄÓ Ó ÑÈÑÒÅÌÀÕ ÄÎÇÓÂÀÍÍß ÏÀËÈÂÀ ÐÎÇÐÎÁÊÈ ÄÏ «ÕÀÊÁ»

ÏÐÈÌÅÍÅÍÈÅ ØÀÃÎÂÎÃÎ ÝËÅÊÒÐÎÏÐÈÂÎÄÀ Â ÑÈÑÒÅÌÀÕ ÄÎÇÈÐÎÂÀÍÈß ÒÎÏËÈÂÀ ÐÀÇÐÀÁÎÒÊÈ ÃÏ «ÕÀÊÁ»

97–100
(4)

Ìåíÿéëîâ Å.Ñ.,
Òðîí÷óê À.À.,
Óãðþìîâà Å.Ì.,
Áàñîâ Þ.Ô.,
Ìåíÿéëîâ À.Â.

METHOD FOR DETERMINING THE LAW ON TILTGuide Vanes of multistage axial COMPRESSORS UNDER UNCERTAINTY OF INPUT DATA

ÌÅÒÎÄ ÂÈÇÍÀ×ÅÍÍß ÇÀÊÎÍÓ ÐÅÃÓËÞÂÀÍÍß ÏÎÂÎÐÎÒÍÈÌÈ ÍÀÏÐÀÂËßÞ×ÈÌÈ ÀÏÀÐÀÒÀÌÈ ÁÀÃÀÒÎÑÒÓϲÍ×ÀÑÒÎÃÎ ÎÑÜÎÂÎÃÎ ÊÎÌÏÐÅÑÎÐÀ  ÓÌÎÂÀÕ ÍÅÂÈÇÍÀ×ÅÍÎÑÒ² ÂÕ²ÄÍÈÕ ÄÀÍÈÕ

ÌÅÒÎÄ ÎÏÐÅÄÅËÅÍÈß ÇÀÊÎÍÀ ÐÅÃÓËÈÐÎÂÀÍÈß ÏÎÂÎÐÎÒÍÛÌÈ ÍÀÏÐÀÂËßÞÙÈÌÈ ÀÏÏÀÐÀÒÀÌÈ ÌÍÎÃÎÑÒÓÏÅÍ×ÀÒÎÃÎ ÎÑÅÂÎÃÎ ÊÎÌÏÐÅÑÑÎÐÀ  ÓÑËÎÂÈßÕ ÍÅÎÏÐÅÄÅËÅÍÍÎÑÒÈ ÂÕÎÄÍÛÕ ÄÀÍÍÛÕ

101–106
(6)

Òàðàñåíêî À.È.,
Òàðàñåíêî À.À.

DETAILS OF DIGITAL CONTROL FOR POWER PLANT GTE ON STARTING AND OPERATING MODES

îñîáëèâîñò³ öèôðîâîãî ðåãóëþâàííÿ ÃÒÄ äëÿ åëåêòðîñòàíö³¿ íà ïóñêîâÈõ òà ðîáî÷èõ ðåæèìàõ

ÎÑÎÁÅÍÍÎÑÒÈ ÖÈÔÐÎÂÎÃÎ ÐÅÃÓËÈÐÎÂÀÍÈß ÃÒÄ ÄËß ÝËÅÊÒÐÎÑÒÀÍÖÈÈ ÍÀ ÏÓÑÊÎÂÛÕ È ÐÀÁÎ×ÈÕ ÐÅÆÈÌÀÕ

107–111
(5)

Kasianov V.A.,
Goncharenko A.V.

SUBJECTIVELY PREFERRED OPTIMALLY CONTROLLED MODES OF OPERATION FOR AN AIRCRAFT MAXIMAL DURATION HORIZONTAL FLIGHT

ÎÏÒÈÌÀËÜÍÎ ÊÅÐÎÂÀͲ ÑÓÁ’ªÊÒÈÂÍÎ ÏÅÐÅÂÀÆÍ² ÐÅÆÈÌÈ ÅÊÑÏËÓÀÒÀÖ²¯ ÃÎÐÈÇÎÍÒÀËÜÍÎÃÎ ÏÎËÜÎÒÓ Ë²ÒÀÊÀ ÌÀÊÑÈÌÀËÜÍί ÒÐÈÂÀËÎÑÒ²

ÎÏÒÈÌÀËÜÍÎ ÓÏÐÀÂËßÅÌÛÅ ÑÓÁÚÅÊÒÈÂÍÎ ÏÐÅÄÏÎ×ÈÒÀÅÌÛÅ ÐÅÆÈÌÛ ÝÊÑÏËÓÀÒÀÖÈÈ ÃÎÐÈÇÎÍÒÀËÜÍÎÃÎ ÏÎËÅÒÀ ÑÀÌÎËÅÒÀ ÌÀÊÑÈÌÀËÜÍÎÉ ÏÐÎÄÎËÆÈÒÅËÜÍÎÑÒÈ

112–117
(6)

Ìèðãîðîä Â.Ô.,
Ãîãóíñêèé Â.Ä.,
Áóðÿ÷åíêî À.Ã.,
Ãðóäèíêèí Â.Ì.

ACCURACY EVALUATION OF GTE PIECE WISE-LINEAR DYNAMIC MODELS

ÎÖ²ÍÊÀ ÒÎ×ÍÎÑÒ² ÊÓÑÊÎÂÎ-˲ͲÉÍÈÕ ÄÈÍÀ̲×ÍÈÕ ÌÎÄÅËÅÉ ÃÒÄ

ÎÖÅÍÊÀ ÒÎ×ÍÎÑÒÈ ÊÓÑÎ×ÍÎ-ËÈÍÅÉÍÛÕ ÄÈÍÀÌÈ×ÅÑÊÈÕ ÌÎÄÅËÅÉ ÃÒÄ

118–121
(4)

Õîðÿê Í.Â.,
Íèêîëàåâ À.Ä.,
Äîëãîïîëîâ Ñ.È.

PARAMETRIC IDENTIFICATION OF A MATHEMATICAL MODEL OF THE LOW-FREQUENCY DYNAMICS PUMPS OF LIQUID ROCKET ENGINES

ÏÀÐÀÌÅÒÐÈ×íà ²ÄÅÍÒÈÔ²ÊÀÖ²ß ìàòåìàòè÷Íί ìîäåë² ÍÈÇÜÊÎ×ÀÑÒÎÒÍί äèíàì²êè øíåêî²ÄÖÅÍÒÐÎÂÈÕ íàñîñ²Â вÄÈÍÍÈÕ ÐÀÊÅÒÍÈÕ ÄÂÈÃÓͲÂ

ÏÀÐÀÌÅÒÐÈ×ÅÑÊÀß ÈÄÅÍÒÈÔÈÊÀÖÈß ÌÀÒÅÌÀÒÈ×ÅÑÊÎÉ ÌÎÄÅËÈ ÍÈÇÊÎ×ÀÑÒÎÒÍÎÉ ÄÈÍÀÌÈÊÈ ØÍÅÊÎÖÅÍÒÐÎÁÅÆÍÛÕ ÍÀÑÎÑΠÆÈÄÊÎÑÒÍÛÕ ÐÀÊÅÒÍÛÕ ÄÂÈÃÀÒÅËÅÉ

122–127
(6)

Åïèôàíîâ Ñ.Â.,
Ñèðåíêî Ô.Ô.,
Ãîëîâèí È.È.

OVERVIEW OF METHODS FOR SYNTHESIZING MATHEMATICAL MODELS OF GAS TURBINE ENGINES AT SUB-IDLE MODES

Àíàë³ç ÌÅÒÎÄÈÊ ÑÈÍÒÅÇÓ ÌÀÒÅÌÀÒÈ×ÍÈÕ ÌÎÄÅËÅÉ ÃÀÇÎÒÓÐÁ²ÍÍÈÕ ÄÂÈÃÓͲ ÍÀ ÅÒÀϲ ÇÀÏÓÑÊÓ

ÀÍÀËÈÇ ÌÅÒÎÄÈÊ ÑÈÍÒÅÇÀ ÌÀÒÅÌÀÒÈ×ÅÑÊÈÕ ÌÎÄÅËÅÉ ÃÀÇÎÒÓÐÁÈÍÍÛÕ ÄÂÈÃÀÒÅËÅÉ ÍÀ ÝÒÀÏÅ ÇÀÏÓÑÊÀ

128–135
(8)

Áàõìåò ß.Ã.

BuilDING FLOW CHaracteristic of flow controller LJE

ÏÎÁÓÄÎÂÀ âèòðàòíî¿ õàðàêòåðèñòèêè ðåãóëÿòîð³â âèòðàò ÆÐÄ

ÏÎÑÒÐÎÅÍÈÅ ÐÀÑÕÎÄÍÎÉ ÕÀÐÀÊÒÅÐÈÑÒÈÊÈ ÐÅÃÓËßÒÎÐÀ ÐÀÑÕÎÄÀ ÆÐÄ

136–140
(5)

Àíòîíîâ À.Î.,
Òðîôèìåíêî Ð.À.,
ßöêî Ë.Ë.,
Ñóòêîâîé À.Î.

MODERN METHODS OF DIAGNOSIS AND CONTROL OF GAS TURBINE AIRCRAFT ENGINES

ÑÓ×ÀÑͲ ÌÅÒÎÄÈ ÊÎÍÒÐÎËÞ ÒÀ IJÀÃÍÎÑÒÓÂÀÍÍß ÃÀÇÎÒÓÐÁ²ÍÍÈÕ À²ÀÖ²ÉÍÈÕ ÄÂÈÃÓͲÂ

ÑÎÂÐÅÌÅÍÍÛÅ ÌÅÒÎÄÛ ÊÎÍÒÐÎËß È ÄÈÀÃÍÎÑÒÈÊÈ ÃÀÇÎÒÓÐÁÈÍÍÛÕ ÀÂÈÀÖÈÎÍÍÛÕ ÄÂÈÃÀÒÅËÅÉ

141–145
(5)

Åïèôàíîâ Ñ.Â.,
Ùåðáàíü Á.À.,
Òîâñòèê À.Â.,
Áàãàóòäèíîâ Í.Ä.,
×åðêàñîâ Þ.Â.

ON-GROUND AUTOMATED DIAGNOSIS COMPLEX FOR TURBOFAN

ÍÀÇÅÌÍÈÉ ÀÂÒÎÌÀÒÈÇÎÂÀÍÈÉ ÊÎÌÏËÅÊÑ Ä²ÀÃÍÎÑÒÈÊÈ ÒÓÐÁÎÐÅÀÊÒÈÂÍÎÃÎ ÄÂÎÕÊÎÍÒÓÐÍÎÃÎ ÄÂÈÃÓÍÀ

ÍÀÇÅÌÍÛÉ ÀÂÒÎÌÀÒÈÇÈÐÎÂÀÍÍÛÉ ÊÎÌÏËÅÊÑ ÄÈÀÃÍÎÑÒÈÊÈ ÒÓÐÁÎÐÅÀÊÒÈÂÍÎÃÎ ÄÂÓÕÊÎÍÒÓÐÍÎÃÎ ÄÂÈÃÀÒÅËß

146–153
(8)

Ìàðöåíþê Å.Â.,
Åïèôàíîâ Ñ.Â.,
Êóëèê Ò.Â.

CHOOSING OPTIMAL MODEL OF TEMPERATURE AT COMPRESSOR DISCHARGE SIMULATING FOR MONITORING LIFETIME EXHAUSTION OF MAIN PARTS OF THREE-SPOOL TFE

ÂÈÁ²Ð ÌÎÄÅ˲ ÄËß ÂÈÇÍÀ×ÅÍÍß ÒÅÌÏÅÐÀÒÓÐÈ ÇÀ ÊÎÌÏÐÅÑÎÐÎÌ ÏÐÈ ÌÎͲÒÎÐÈÍDz ÂÈ×ÅÐÏÀÍÍß ÐÅÑÓÐÑÓ ÎÑÍÎÂÍÈÕ ÄÅÒÀËÅÉ ÒÐÜÎÕÂÀËÜÍÎÃÎ ÒÐÄÄ

ÂÛÁÎÐ ÌÎÄÅËÈ ÄËß ÎÏÐÅÄÅËÅÍÈß ÒÅÌÏÅÐÀÒÓÐÛ ÇÀ ÊÎÌÏÐÅÑÑÎÐÎÌ ÏÐÈ ÌÎÍÈÒÎÐÈÍÃÅ ÂÛÐÀÁÎÒÊÈ ÐÅÑÓÐÑÀ ÎÑÍÎÂÍÛÕ ÄÅÒÀËÅÉ ÒÐÅÕÂÀËÜÍÎÃÎ ÒÐÄÄ

154–160
(7)

Âàðáàíåö Ð.À.,
Êó÷åðåíêî Þ.Í.,
Ãîëîâàíü À.È.,
Àëåêñàíäðîâñêàÿ Í.È.

ÂËÈßÍÈÅ ÑÈÑÒÅÌÛ VIT ÍÀ ÕÀÐÀÊÒÅÐ ÐÀÁÎ×ÅÃÎ ÏÐÎÖÅÑÑÀ ÌÀËÎÎÁÎÐÎÒÍÛÕ ÄÈÇÅËÅÉ  MAN-B&W ÑÅÐÈÈ MC

ÂÏËÈ ÑÈÑÒÅÌÛ VIT ÍÀ ÕÀÐÀÊÒÅÐ ÐÎÁÎ×ÎÃÎ ÏÐÎÖÅÑÓ ÌÀËÎÎÁÅÐÒÎÂÈÕ ÄÈÇÅ˲  MAN-B&W ÑÅв¯ MC

ÂËÈßÍÈÅ ÑÈÑÒÅÌÛ VIT ÍÀ ÕÀÐÀÊÒÅÐ ÐÀÁÎ×ÅÃÎ ÏÐÎÖÅÑÑÀ ÌÀËÎÎÁÎÐÎÒÍÛÕ ÄÈÇÅËÅÉ  MAN B&W ÑÅÐÈÈ MC

161–165
(5)

Çàðåìáà Ý.Â.,
Êîâàëåâ È.Ï.

RESEARCH OF VIBRATION CHARACTERISTICS OF ENGINE D-436TP FAN ON BE-200ES AMPHIBIAN IN ICING CONDITIONS

ÄÎÑË²ÄÆÅÍÍß Â²ÁÐÀÖ²ÉÍÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÂÅÍÒÈËßÒÎÐÀ ÄÂÈÃÓÍÀ Ä-436òï ÍÀ ˲ÒÀÊÓ-ÀÌÔ²Á²¯ ÁÅ-200×Ñ Ï³ä ÷àñ ÎÁÌÅÐÇÀÍÍß

ÈÑÑËÅÄÎÂÀÍÈÅ ÂÈÁÐÀÖÈÎÍÍÛÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÄÂÈÃÀÒÅËß Ä-436ÒÏ ÍÀ ÑÀÌÎËÅÒÅ-ÀÌÔÈÁÈÈ ÁÅ-200×Ñ ÂÎ ÂÐÅÌß ÎÁËÅÄÅÍÅÍÈß

166–170
(5)

Áóðàó Í.È.,
Ïàâëîâñêèé À.Ì.,
ßöêî Ë.Ë.,
Èâàí÷åíêî À.Â.

DEVELOPMENT AND INVESTIGATION OF THE DIGITAL TRACKING FILTERS FOR THE VIBRATION CONTROL SYSTEM OF AVIATION ENGINE AT TE NON-STEADY-STATE MODES

ÐÎÇÐÎÁÊÀ ÒÀ ÄÎÑË²ÄÆÅÍÍß ÖÈÔÐÎÂÈÕ Ñ˲ÄÊÓÞ×ÈÕ Ô²ËÜÒв ÄËß ÑÈÑÒÅÌÈ ÊÎÍÒÐÎËÞ Â²ÁÐÀÖ²¯ À²ÀÖ²ÉÍÎÃÎ ÄÂÈÃÓÍÀ ÍÀ ÍÅÑÒÀÖ²ÎÍÀÐÍÈÕ ÐÅÆÈÌÀÕ

ÐÀÇÐÀÁÎÒÊÀ È ÈÑÑËÅÄÎÂÀÍÈÅ ÖÈÔÐÎÂÛÕ ÑËÅÄßÙÈÕ ÔÈËÜÒÐÎÂ ÄËß ÑÈÑÒÅÌÛ ÊÎÍÒÐÎËß ÂÈÁÐÀÖÈÈ ÀÂÈÀÖÈÎÍÍÎÃÎ ÄÂÈÃÀÒÅËß ÍÀ ÍÅÑÒÀÖÈÎÍÀÐÍÛÕ ÐÅÆÈÌÀÕ

171–176
(6)

Þð Ò.Â.,
Õàðèòîíîâ Â.Ì.,
Äóáðîâ³í Â.².

MODEL FOR EVALUATION OF GAS-TURBINE ENGINE ELEMENTS TECHNICAL STATE BY VIBRATION PARAMETERS BASED ON WAVELET-TRANSFOR

ÌÎÄÅËÜ ÎÖ²ÍÊÈ ÒÅÕͲ×ÍÎÃÎ ÑÒÀÍÓ ÂÓÇ˲ ÃÒÄ ÇÀ ÏÀÐÀÌÅÒÐÀÌÈ Â²ÁÐÀÖ²¯ Ç ÂÈÊÎÐÈÑÒÀÍÍßÌ ÂÅÉÂËÅÒ-ÏÅÐÅÒÂÎÐÅÍÍß

ÌÎÄÅËÜ ÎÖÅÍÊÈ ÒÅÕÍÈ×ÅÑÊÎÃÎ ÑÎÑÒÎßÍÈß ÓÇËΠÃÒÄ ÏÎ ÏÀÐÀÌÅÒÐÀÌ ÂÈÁÐÀÖÈÈ Ñ ÏÐÈÌÅÍÅÍÈÅÌ ÂÅÉÂËÅÒ-ÏÐÅÎÁÐÀÇÎÂÀÍÈß

177–182
(6)

Øóëüæåíêî Í.Ã.,
Åôðåìîâ Þ.Ã.,
Öûáóëüêî Â.È.,
Äåïàðìà À.Â.

APPLICATION OF METHODS AND MEANS OF VIBRATION DIAGNOSTICS FOR THE ESTIMATION OF RELIABILITY OF WORK OF TURBINE SETS

ÇÀÑÒÎÑÓÂÀÍÍß ÌÅÒÎIJ ² ÇÀÑÎÁ²Â ²ÁÐÎIJÀÃÍÎÑÒÈÊÈ ÄËß ÎÖ²ÍÊÈ ÍÀIJÉÍÎÑÒ² ÐÎÁÎÒÈ ÒÓÐÁÎÀÃÐÅÃÀÒ²Â

ÏÐÈÌÅÍÅÍÈÅ ÌÅÒÎÄÎÂ È ÑÐÅÄÑÒÂ ÂÈÁÐÎÄÈÀÃÍÎÑÒÈÊÈ ÄËß ÎÖÅÍÊÈ ÍÀÄÅÆÍÎÑÒÈ ÐÀÁÎÒÛ ÒÓÐÁÎÀÃÐÅÃÀÒÎÂ

183–188
(6)

Ðåçíèê Ñ.Á.,
Áàíäóðêî Å.À.

SETTLEMENT AND EXPERIMENTAL EVALUATION different types of labyrinth seals

ÐÎÇÐÀÕÓÍÊÎÂÎ-ÅÊÑÏÅÐÈÌÅÍÒÀËÜÍÀ ÎÖ²ÍÊÀ ÅÔÅÊÒÈÂÍÎÑÒ² вÇÍÈÕ ÒÈϲ ËÀÁ²ÐÈÍÒÎÂÈÕ ÓÙ²ËÜÍÅÍÜ

ÐÀÑרÒÍÎ-ÝÊÑÏÅÐÈÌÅÍÒÀËÜÍÀß ÎÖÅÍÊÀ ÝÔÔÅÊÒÈÂÍÎÑÒÈ ÐÀÇËÈ×ÍÛÕ ÒÈÏΠËÀÁÈÐÈÍÒÍÛÕ ÓÏËÎÒÍÅÍÈÉ

189–193
(
5)

Èíôîðìàöèîííûå òåõíîëîãèè

Äàíîâ À.Ñ.

INFORMATION ENERGY APPROACH TO PROJECTION PROBLEM

²ÍÔÎÐÌÀÖ²ÉÍÎ-ÅÍÅÐÃÅÒÈ×ÍÈÉ Ï²ÄÕ²Ä ÄÎ ÏÐÎÁËÅÌÈ ÏÐÎÅÊÒÓÂÀÍÍß

ÈÍÔÎÐÌÀÖÈÎÍÍÎ-ÝÍÅÐÃÅÒÈ×ÅÑÊÈÉ ÏÎÄÕÎÄ Ê ÏÐÎÁËÅÌÅ ÏÐÎÅÊÒÈÐÎÂÀÍÈß

194–198
(5)

Ëåùåíêî Þ.Ï.

INTELLECTUAL CONTROL SYSTEM BY MEASURING ROBOT

²ÍÒÅËÅÊÒÓÀËÜÍÀ ÑÈÑÒÅÌÀ ÓÏÐÀÂ˲ÍÍß ÂÈ̲ÐÞÂÀËÜÍÈÌ ÐÎÁÎÒÎÌ

ÈÍÒÅËËÅÊÒÓÀËÜÍàÿ ÑÈÑÒÅÌà ÓÏÐÀÂËÅÍÈß ÈÇÌÅÐÈÒÅËÜÍÛÌ ÐÎÁÎÒÎÌ

199–202
(4)

Òàìàðãàç³í Î.À.,
˳íí³ê ².².,
Áîãàéñüêà Ê.Â.,
Êðàìàðåíêî Ò.Þ.

CORRELATION FUNCTIONS OF THE NUMBER OF APPLICATIONS FOR ELIMINATION OF DAMAGES OF POWER PLANTS IN THE OPERATIONAL MAINTENANCE

ÊÎÐÅËßÖ²ÉͲ ÔÓÍÊÖ²¯ ʲËÜÊÎÑÒ² ÇÀßÂÎÊ ÍÀ ÓÑÓÍÅÍÍß ÏÎØÊÎÄÆÅÍÜ ÑÈËÎÂÈÕ ÓÑÒÀÍÎÂÎÊ Ó ÏÐÎÖÅѲ ÎÏÅÐÀÒÈÂÍÎÃÎ ÒÅÕͲ×ÍÎÃÎ ÎÁÑËÓÃÎÂÓÂÀÍÍß

ÊÎÐÐÅËßÖÈÎÍÍÛÅ ÔÓÍÊÖÈÈ ÊÎËÈ×ÅÑÒÂÀ ÇÀßÂÎÊ ÍÀ ÓÑÒÐÀÍÅÍÈÅ ÏÎÂÐÅÆÄÅÍÈÉ ÑÈËÎÂÛÕ ÓÑÒÀÍÎÂÎÊ Â ÏÐÎÖÅÑÑÅ ÎÏÅÐÀÒÈÂÍÎÃÎ ÒÅÕÍÈ×ÅÑÊÎÃÎ ÎÁÑËÓÆÈÂÀÍÈß

203–207
(5)

ßêóøåíêî Î.Ñ.,
̳ëüöîâ Â.ª.,
Éîâåíêî Ñ.².,
Ðàòèíñüêèé Â.Â.,
×óìàê Î.².

THE AUTOMATED MONITORING OF RELIABILITY IN AIRLINE

ÀÂÒÎÌÀÒÈÇÎÂÀÍÈÉ ÌÎͲÒÎÐÈÍà ÍÀIJÉÍÎÑÒ² ÍÀ вÂͲ À²ÀÊÎÌÏÀͲ¯

ÀÂÒÎÌÀÒÈÇÈÐÎÂÀÍÍÛÉ ÌÎÍÈÒÎÐÈÍÃ ÍÀÄÅÆÍÎÑÒÈ ÍÀ ÓÐÎÂÍÅ ÀÂÈÀÊÎÌÏÀÍÈÈ

208–213
(6)

Ðåâà Î.Ì.,
Áîðñóê Ñ.Ï.

FUZZY MODEL OF AIR TRAFFIC CONTROLLERS ATTITUDE TO THE RISK OF POTENTIAL CONFLICTS SITUATION APPEARANCE

ÍÅײÒÊÀ ÌÎÄÅËÜ ÑÒÀÂËÅÍÍß À²ÀÄÈÑÏÅÒ×ÅÐÀ ÄÎ ÐÈÇÈÊÓ ÍÀÑÒÀÍÍß ÏÎÒÅÍÖ²ÉÍÎ-ÊÎÍÔ˲ÊÒÍί ÑÈÒÓÀÖ²¯

ÍÅ×ÅÒÊÀß ÌÎÄÅËÜ ÎÒÍÎØÅÍÈß ÀÂÈÀÄÈÑÏÅÒ×ÅÐÀ Ê ÐÈÑÊÓ ÍÀÑÒÓÏËÅÍÈß ÏÎÒÅÍÖÈÀËÜÍÎ ÊÎÍÔËÈÊÒÍÎÉ ÑÈÒÓÀÖÈÈ

214–221
(8)

Õîìÿê Î.Â.

ASSESSMENT OF LOSS IN RADIO PROPAGATION MODEL FOR POINT-TO-POINT FOR REFLECTION FROM LOCAL ITEMS

ÎÖ²ÍÊÀ ÂÒÐÀÒ ÐÀIJÎÑÈÃÍÀËÓ ÏÐÈ ÏÎØÈÐÅÍͲ  ÌÎÄÅ˲ POINT-TO-POINT ÇÀ ÐÀÕÓÍÎÊ Â²ÄÁÈÒÒß Â²Ä Ì²ÑÖÅÂÈÕ ÏÐÅÄÌÅÒ²Â

ÎÖÅÍÊÀ ÏÎÒÅÐÜ ÐÀÄÈÎÑÈÃÍÀËÀ ÏÐÈ ÐÀÑÏÐÎÑÒÐÀÍÅÍÈÈ Â ÌÎÄÅËÈ POINT-TO-POINT ÇÀ Ñ×ÅÒ ÎÒÐÀÆÅÍÈß ÎÒ ÌÅÑÒÍÛÕ ÏÐÅÄÌÅÒÎÂ

222–225
(4)

Áóòåíêî Þ.È.

METHOD MACHINE PROCESSING LANGUAGE UNITS IN THE CLASS «LANGUAGE SOFTWARE STANDARDS»

ÌÅÒÎÄÈÊÀ ÌÀØÈÍÍί ÎÁÐÎÁÊÈ Ë²ÍòÑÒÈ×ÍÈÕ ÎÄÈÍÈÖÜ ÊËÀÑÓ «ÌÎÂÀ ÑÒÀÍÄÀÐҲ ÏÐÎÃÐÀÌÍÎÃÎ ÇÀÁÅÇÏÅ×ÅÍÍß»

ÌÅÒÎÄÈÊÀ ÌÀØÈÍÍÎÉ ÎÁÐÀÁÎÒÊÈ ËÈÍÃÂÈÑÒÈ×ÅÑÊÈÕ ÅÄÈÍÈÖ ÊËÀÑÑÀ «ßÇÛÊ ÑÒÀÍÄÀÐÒΠÏÐÎÃÐÀÌÌÍÎÃÎ ÎÁÅÑÏÅ×ÅÍÈß»

226–230
(5)

Øóëüã³í Â.À.

INDISTINCT ENTHROPY AS A MEASURE OF PILOTING PRECISION APPRAISAL DISTINCTION, MADE BY PILOTS

ÍÅײÒÊÀ ÅÍÒÐÎÏ²ß ßÊ Ì²ÐÀ ÐÎÇϲÇÍÀÂÀÍÍß Ï²ËÎÒÀÌÈ ÎÖ²ÍÎÊ ÒÎ×ÍÎÑÒ² ϲËÎÒÓÂÀÍÍß

ÍÅ×ÅÒÊÀß ÝÍÒÐÎÏÈß ÊÀÊ ÌÅÐÀ ÐÀÑÏÎÇÍÀÂÀÍÈß ÏÈËÎÒÀÌÈ ÎÖÅÍÎÊ ÒÎ×ÍÎÑÒÈ ÏÈËÎÒÈÐÎÂÀÍÈß

231–235
(5)

Êó÷óê Ã.À.

MULTISERVICE NETWORK SECTION TRAFFIC IS CONTROLLED

ÓÏÐÀÂ˲ÍÍß ÒÐÀÔ²ÊÎÌ ëàíêè ìóëüòèñåðâ³ñíî¯ ìåðåæ³

ÓÏÐÀÂËÅÍÈÅ ÒÐÀÔÈÊÎÌ ÇÂÅÍÀ ÌÓËÜÒÈÑÅÐÂÈÑÍÎÉ ÑÅÒÈ

236–239
(4)

Ðåâà Â.Ñ.,
Ôðîëîâ Â.Ï.,
Çåìëÿíîé Ê.Í.

DEFINITION OF THE OFF-NOMINAL SITUATIONS AND METHODS OF THEIR MANAGEMENT AT THE STAGES OF GROUND COMPLEX POWER-SUPPLY SYSTEMS OPERATION

ÂÈÇÍÀ×ÅÍÍß ÍÅØÒÀÒÍÈÕ ÑÈÒÓÀÖ²É ÒÀ ÌÅÒÎIJ ¯Õ ÓÑÓÍÅÍÍß ÍÀ ÅÒÀÏÀÕ ÅÊÑÏËÓÀÒÀÖ²¯ ÑÈÑÒÅÌ ÅËÅÊÒÐÎÏÎÑÒÀ×ÀÍÍß ÍÀÇÅÌÍÎÃÎ ÊÎÌÏËÅÊÑÓ

ÎÏÐÅÄÅËÅÍÈÅ ÍÅØÒÀÒÍÛÕ ÑÈÒÓÀÖÈÉ È ÌÅÒÎÄÎÂ ÈÕ ÏÀÐÈÐÎÂÀÍÈß ÍÀ ÝÒÀÏÀÕ ÝÊÑÏËÓÀÒÀÖÈÈ ÑÈÑÒÅÌ ÝËÅÊÒÐÎÑÍÀÁÆÅÍÈß ÍÀÇÅÌÍÎÃÎ ÊÎÌÏËÅÊÑÀ

240–243
(4)

Èíôîðìàöèîííûå òåõíîëîãèè â óïðàâëåíèè ïðåäïðèÿòèÿìè, ïðîãðàììàìè è ïðîåêòàìè

Âîëêîâ Ä.È.,
Âîëîøèíà Í.Ï.,
Ðàí÷åíêî Ã.Ñ.

CALLS OF THE MARKET. THE DEVELOPMENT STRATEGY OF THE AVIONICS ENTERPRISE

ÂÈÊËÈÊÈ ÐÈÍÊÓ. ÑÒÐÀÒÅÃ²ß ÐÎÇÂÈÒÊÓ Ï²ÄÏÐȪÌÑÒÂÀ-ÐÎÇÐÎÁÍÈÊÀ À²ÀÖ²ÉÍί ÅËÅÊÒÐÎͲÊÈ

ÂÛÇÎÂÛ ÐÛÍÊÀ. ÑÒÐÀÒÅÃÈß ÐÀÇÂÈÒÈß ÏÐÅÄÏÐÈßÒÈß-ÐÀÇÐÀÁÎÒ×ÈÊÀ ÀÂÈÀÖÈÎÍÍÎÉ ÝËÅÊÒÐÎÍÈÊÈ

244–248
(5)

Äàâèäåíêî Â.Î.

INFORMATION TECHNOLOGY OF SUPPORT OF DECISION-MAKING ON POPULATION EVACUATION FROM THE ZONE OF EMERGENCY SITUATIONS OF ANTHROPOGENIC CHARACTER

²ÍÔÎÐÌÀÖ²ÉÍÀ ÒÅÕÍÎËÎÃ²ß Ï²ÄÒÐÈÌÊÈ ÏÐÈÉÍßÒÒß Ð²ØÅÍÜ Ç ÅÂÀÊÓÀÖ²¯ ÍÀÑÅËÅÍÍß ²Ç ÇÎÍÈ íàäçâè÷àéíèõ ñèòóàö³é òåõíîãåííîãî õàðàêòåðó

ÈÍÔÎÐÌÀÖÈÎÍÍÀß ÒÅÕÍÎËÎÃÈß ÏÎÄÄÅÐÆÊÈ ÏÐÈÍßÒÈß ÐÅØÅÍÈÉ ÏÎ ÝÂÀÊÓÀÖÈÈ ÍÀÑÅËÅÍÈß ÈÇ ÇÎÍÛ ×ÐÅÇÂÛ×ÀÉÍÛÕ ÑÈÒÓÀÖÈÉ ÒÅÕÍÎÃÅÍÍÎÃÎ ÕÀÐÀÊÒÅÐÀ

249–253
(5)

Ïîòàïîâà Ì.Â.

INFORMATION TECHNOLOGY OF SCHEDULING IN CASE OF PORTFOLIO MANAGEMENT OF ORDERS OF THE IT COMPANY IN THE CONDITIONS OF UNCERTAINTY

²ÍÔÎÐÌÀÖ²ÉÍÀ ÒÅÕÍÎËÎÃ²ß ÊÀËÅÍÄÀÐÍÎÃÎ ÏËÀÍÓÂÀÍÍß ÏÐÈ ÓÏÐÀÂ˲ÍͲ ÏÎÐÒÔÅËÅÌ ÇÀÌÎÂËÅÍÜ IT-ÊÎÌÏÀͲ¯  ÓÌÎÂÀÕ ÍÅÂÈÇÍÀ×ÅÍÎÑÒ²

ÈÍÔÎÐÌÀÖÈÎÍÍÀß ÒÅÕÍÎËÎÃÈß ÊÀËÅÍÄÀÐÍÎÃÎ ÏËÀÍÈÐÎÂÀÍÈß ÏÐÈ ÓÏÐÀÂËÅÍÈÈ ÏÎÐÒÔÅËÅÌ ÇÀÊÀÇÎÂ IT-ÊÎÌÏÀÍÈÈ Â ÓÑËÎÂÈßÕ ÍÅÎÏÐÅÄÅËÅÍÍÎÑÒÈ

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Óâàæàåìûå ÷èòàòåëè!

Íàó÷íî-òåõíè÷åñêèé æóðíàë «Àâèàöèîííî-êîñìè÷åñêàÿ òåõíèêà è òåõíîëîãèÿ»

- âõîäèò â óòâåðæäåííûé ÃÀÊ Ïåðå÷åíü íàó÷íûõ ïðîôåññèîíàëüíûõ èçäàíèé Óêðàèíû, â êîòîðûõ ìîãóò ïóáëèêîâàòüñÿ ðåçóëüòàòû äèññåðòàöèîííûõ ðàáîò íà ñîèñêàíèå ó÷åíûõ ñòåïåíåé äîêòîðà è êàíäèäàòà íàóê (ñì. ïîñòàíîâëåíèå ïðåçèäèóìà ÂÀÊ Óêðàèíû ¹1-05/4 îò 14.10.2009 ã.);

– ñîõðàíÿåòñÿ â îáùåãîñóäàðñòâåííîé ðåôåðàòèâíîé áàçå äàííûõ «Óêðà¿í³êà íàóêîâà» è ïóáëèêóåòñÿ â ñîîòâåòñòâóþùèõ òåìàòè÷åñêèõ ñåðèÿõ óêðàèíñêîãî ðåôåðàòèâíîãî æóðíàëà «Äæåðåëî» (ñâîáîäíûé îí-ëàéíîâûé äîñòóï ê ðåñóðñàì íà Web-ñåðâåðå http://www.nbuv.gov.ua) (Óêðàèíà),

– ñîõðàíÿåòñÿ â ðåôåðàòèâíîé áàçå äàííûõ Âñåðîññèéñêîãî èíñòèòóòà íàó÷íîé è òåõíè÷åñêîé èíôîðìàöèè (ÂÈÍÈÒÈ) Ðîññèéñêîé àêàäåìèè íàóê è ïóáëèêóåòñÿ â ñîîòâåòñòâóþùèõ òåìàòè÷åñêèõ ñåðèÿõ ÐÆ (ñâîáîäíûé îí-ëàéíîâûé äîñòóï ê ðåñóðñàì íà Web-ñåðâåðå http://www.viniti.ru) (Ðîññèéñêàÿ Ôåäåðàöèÿ),

- âêëþ÷åí â ìåæäóíàðîäíûå íàóêîìåòðè÷åñêèå áàçû äàííûõ: íàó÷íîé ýëåêòðîííîé áèáëèîòåêè eLIBRARY.RU (Ðîññèéñêàÿ Ôåäåðàöèÿ); Index Copernicus (Ïîëüøà); Google Scholar.