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THE SCHEME OF SIMULATION CASES FOR MATHEMATICAL MODELING OF HELICOPTER DYNAMICS WITH THE CARGO ON THE EXTERNAL SLING AT TAKEOFF AND LANDING PHASES

Abstract

When a helicopter performs an air operation and aerial work using external sling there may occur special situations, as the result of unfavourable conditions impact. The most difficult and dangerous stages of flight are the takeoff and landing.To study an aircraft flight dynamics in extreme flight conditions, including a helicopter with cargo on external sling, the most effective is to use the theoretical methods, mathematical modeling in particular, which is relatively cheap, able to model the abnormal situation including disasters, and able to set the necessary environ-mental effect.During the theoretical studies it is impractical and impossible to simulate all the abnormal situations that may occur at the given phases of flight. Therefore, at the initial stage of the research it is necessary to deal with making up a list of the most typical abnormal situations - the scheme of simulation cases. This issue is the subject of this article.The article describes the typical errors of piloting a helicopter with cargo on external sling at takeoff and landing, as well as the most dangerous equipment failures and noncalculated operating conditions, based on the analysis of which the scheme of simulation cases has been made. After modeling in accordance with the scheme of simulation cases, it will be possible to determine the effect of the cargo parameters, flight parameters, the impact of unfavourable factors on the dynamics of the system "helicopter - cargo on external sling" at takeoff and landing, which theefore will determine the boundaries of the system safe operation on these phases of flight, and to formulate recommendations for the crew to prevent abnomal situations or to get out of them.For further research it is expected to use the earlier developed HeliCargo software application, which allows to simulate the dynamics of helicopter with cargo on external sling.

About the Authors

V. V. Efimov
Moscow State Technical University of Civil Aviation
Russian Federation

Doctor of Science, Associate Professor, Professor,

Moscow



A. Elsaidabdo
Moscow State Technical University of Civil Aviation
Russian Federation

Externa PhD Student,

Moscow



References

1. Efimov V.V. Osobennosti obespechenija bezopasnosti jekspluatacii vertoletov s gruzom na vneshnej podveske [Features of Providing of Helicopters Exploitation Safety with Cargo on External Sling]. Nauchnyi Vestnik MGTU GA [Scientific Bulletin of MSTUCA], 2010, no. 151, pp. 124–129. (in Russian)

2. Doc 9859. Safety Management Manual (SMM). ICAO. 2013. 251 p.

3. Efimov V.V., Parshentsev S.A. Rezul'taty vychislitel'nyh jeksperimentov po issledovaniju dinamiki vertoleta i gruza na ego vneshnej trosovoj podveske pri polete v nespokojnom vozduhe [The Results of the Mathematical Flight Simulation of the Helicopter with the Cargo on the External Sling]. Nauchnyi Vestnik MGTU GA [Scientific Bulletin of MSTUCA], 2008, no. 125, pp. 151–158. (in Russian)

4. Efimov V.V. Issledovanie vlijanija parametrov gruza na uslovija ego ravnovesija na vneshnej podveske vertoleta [Research of Influence of Cargo Parameters on Conditions of its Balance on the Helicopter External Sling]. Nauchnyi Vestnik MGTU GA [Scientific Bulletin of MSTUCA], 2010, no. 151, pp. 130–137. (in Russian)

5. Efimov V.V. O vlijanii gruza na vneshnej podveske vertoleta na ego ravnovesie [Effect of Cargo on External Sling Helicopter on its Equilibrium]. Nauchnyi Vestnik MGTU GA [Scientific Bulletin of MSTUCA], 2010, no. 154, pp. 79–85. (in Russian)

6. Efimov V.V., Ivchin V.A. Issledovanie vlijanija parametrov gruza na vneshnej podveske na balansirovochnye harakteristiki vertoleta [Investigation of the Influence of Parameters Cargo on External Sling on the Balancing Data Helicopter] Nauchnyi vestnik MGTU GA. [Scientific Bulletin of MSTUCA], 2010, no. 154, pp. 86–93. (in Russian)

7. Efimov V.V. Dinamicheskaja ustojchivost' gruza na trosovoj vneshnej podveske vertoleta [Investigation of the Dynamic Stability of Cargo on the Helicopter External Sling]. Obshherossijskij nauchno-tehnicheskij zhurnal "Polet" [POLYOT All-Russian Scientific-Technical Journal], 2011, no. 3, pp. 26–32. (in Russian)

8. Efimov V.V. Avtokolebanija gruzov na trosovoj vneshnej podveske vertoleta [Autooscillations of Cargo on the Helicopter External Sling]. Obshherossijskij nauchno-tehnicheskij zhurnal "Polet" [POLYOT All-Russian Scientific-Technical Journal], 2011, no. 12, pp. 23–28. (in Russian)

9. Efimov V.V. Issledovanie avtokolebanij vertoleta s gruzom na vneshnej trosovoj podveske [Investigation of Self-Oscillations Helicopter with the Cargo on the External Sling]. Nauchnyi Vestnik MGTU GA [Scientific Bulletin of MSTUCA], 2012, no. 177, pp. 65–71. (in Russian)

10. Efimov V.V., Ivchin V.A. Rezul'taty matematicheskogo modelirovanija dinamiki vertoleta posle sbrosa gruza s ego vneshnej podveski [The Results of Helicopter Dynamics Mathematical Modeling After Discharge of Cargo with its External Sling]. Nauchnyi Vestnik MGTU GA [Scientific Bulletin of MSTUCA], 2016, no. 223, pp. 101–108. (in Russian)

11. Rukovodstvo po letnoj jekspluatacii vertoleta Mi-8MTV: vvedeno v dejstvie otdelom letnoj jekspluatacii Departamenta vozdushnogo transporta Ministerstva transporta Rossijskoj Federacii 14 maja 1994 g. [Flight Crew Operations Manual Mi-8MTV: enacted with Flight Operations Department of Air Transport Department of the Russian Federation Transport Ministry of May 14, 1994], p. 7.11.4. (in Russian)

12. Kozlovsky V.B., Parshentsev S.A., Efimov V.V. Vertolet s gruzom na vneshnej podveske [Helicopter with Cargo on External Sling]. Mashinostroenie / Mashinostroenie – Polet. [Mechanical Engineering / Mechanical Engineering-Flight] Moscow. 2008. 304 p. (in Russian)


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For citations:


Efimov V.V., Elsaidabdo A. THE SCHEME OF SIMULATION CASES FOR MATHEMATICAL MODELING OF HELICOPTER DYNAMICS WITH THE CARGO ON THE EXTERNAL SLING AT TAKEOFF AND LANDING PHASES. Civil Aviation High Technologies. 2016;19(6):17-23. (In Russ.)

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ISSN 2079-0619 (Print)
ISSN 2542-0119 (Online)