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CONTENTS #11-12 (November – December) 2017

Modeling Of Accidents In Aviation Transport Systems Taking Into Account The Human Factor (p. 3 – 10)

G.V. Novozhilov, A.S. Bogomolov, V.A. Ivaschenko, V.A. Kushnikov, M.S. Neymark, A.F. Rezchikov,

E.A. Salina, L.Yu. Filimonyuk, L.G. Tsesarskiy, I.I. Sholomov, K.I. Sholomov

The approach to representation of processes of occurrence and prevention of accidents with participation of the human factor is offered. The mathematical apparatus used is based on the theory of cause-effect complexes, Markov processes and probabilistic safety analysis. The developed mathematical support allows to reveal new variants of critical combinations of technical failures and special states of operators leading to occurrence of emergency situations. An example of the use of the developed security in the case of the aviation-transport system is given.

Keywords: aviation transport system; accident; safety; human factor; critical events’ combinations; event tree.

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The Crew’s Role Over Increasing Scientific Research Effectiveness On The ISS Russian Segment
(p. 11 – 19)

A.Yu. Kalery, A.V. Markov, I.S. Nechayev, V.A. Soloviev, I.V. Sorokin

Аnalyzes the results of the Russian Segment of the International Space Station (ISS RS) utilization, obtained in 2000 –2016, from the standpoint of how crewmembers’ activities affect the effectiveness of the utilization process. The impact of this activity on results of scientific research is also presented. Some recommendations over use of the ISS RS crew experience, associated with research program realization, are provided. An assessment is also made of cosmonauts’ expected contribution to the process of scientific venture during long-duration missions beyond the low Earth orbit.

Keywords: International space station; utilization; scientific and applied research programs; effectiveness increase methods; integrated infomedia; nonconformities.

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Aircraft Flight Safety At Safety At Supermaneuverability Models (p. 20 – 25)

O.A. Balyk

Main directions of tests normative-methodical supporting for evaluation of military aircraft flight safety at supermaneuverability modes are stated in this work. Work results in the sphere of flight safety evaluation in cases of aircraft engine failures at supermaneuverability modes are given here.

Keywords: supermaneuverability mode; calculated case; engine failure.

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The Possibility Of Improving The Accuracy Of Determining Navigation Parameters Of Systems Of Maintenance Of Landing Of The Aircraft With A Digital Optical Means (p. 26 – 30)

V.V. Vasilyev, R.V. Dzhugan, A.P. Manin, V.L. Sokolyuk

Modern digital optical devices have great potential for measuring distances between images of different objects in the image plane. Shows how you can use this property to build systems ensure the landing of aircraft on a narrow spot.

Keywords: the landing system; video; dimension; theodolite; optical system; the source of radiation; coordinates.

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Numerical Method Of Variation Analytical Programming For Structural And Parametrical Synthesis Of A Control System (p. 31 – 37)

A.I. Diveev, N.B. Konyrbaev

The method of structural and parametrical synthesis of a control system, a method of variation analytical programming which differs from the known method of analytical programming in use of the principle of small variations of the basic decision is presented. The description of a structure of data for coding of mathematical expression, small variations of structure and a variation genetic algorithm for search of an optimal solution is provided. The example of the solution of a problem of synthesis of a control system of method of variation analytical programming for object of management of the third order with phase restrictions is given.

Keywords: method of variational analytical programming; synthesis of control system; genetic algorithm.

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Physical Simulation Of Spacecraft Parts Shock Loading (p. 38 – 47)

A.S. Birukov, O.G. Demenko, N.A. Mikhalenkov

Simulation problems of spacecraft parts impact load, specified by shock spectrum, during off-line shock testing is devoted. It is proposed using of single mechanical shocks for this task. Equivalent mechanical shock concept is considered. Procedure of single mechanical shock characteristics definition is validated.

Keywords: shock spectrum; spacecraft shock test; spacecraft shock strength; simulation of bodies shock interaction.

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Study Of The Effect Of An Additional Management Body (Flap) On The Aerodynamic Characteristics Of The Airfoil With The Flap (p. 48 – 53)

A.A. Erokhina, V.P. Erokhin, L.G. Artamonova

Presents the results of a numerical 2D-simulation of the profile with rejected-ness of the flap, and an additional control (the flap). Flap installed remained at 0.25 of the chord on the leeward side of the profile at an angle δ=45°.

Keywords: additional management body (plate); separation of flow; numerical methods; aerodynamic coefficients; the flap.

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Mathematical Simulation Of Plane-Type Descent Module (p. 54 – 59)

A.M. Маtveenko, A.A. Zotov, O.A. Pashkov, A.V. Kuznetsov

The results obtained during the study aerodynamic characteristics of the prototype of a small descent vehicle developed by the staff of the Moscow Aviation Institute are presented. The investigations were carried out using the numerical method developed by the authors, based on the solution of discrete analogs of the Navier-Stokes equations. On the basis of the obtained results, the perspective of the aerodynamic configuration of the descent vehicle, which is based on an ultra-small extension wing, is shown.

Keywords: descent module; mathematical simulation; load-bearing airframe; thermal reentry.

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Integrated Ergonomic Assessment Of A Crew Cabin Of Perspective Combat Aircraft (p. 60 – 65)

D.N. Levin

The integrated approach to the ergonomic evaluation of cockpit advanced aircraft, based on the integration of the stand simulation of different ergonomic parameters.

Keywords: aircraft control and navigational equipment; information pattern; crew station design; ergonomic evaluation; human-computer interface; view from plane.

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The Investment Of Zubec’s EDB-16 In Reliability Of Grushin’s Missile For Anti-aircraft Missille Systems S-300P And S-300F (p. 66 – 73)

D.M. Galperin

This is decision about liquidation periodical burnout of housing serial solid-fuel engine of antiaircraft missile 5V55 Mashine Designe Bureau (MDB) P.D. Grushin’s. Elimination of failures based on experience Zubec’s Experienced Bureau (EDB-16). Experience of EDB-16 based on application of progressive methods composition the compound solid rocket fuels and equipment solid-fuel engines. The missile is successfully operated as part of anti-aircraft missiles systems S-300P and S-300F.

Keywords: anti-aircraft missile system; solid-fuel rocket engine; compound solid rocket fuel.

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