THE RESULTS OF HELICOPTER DYNAMICS MATHEMATICAL MODELING AFTER DISCHARGE OF CARGO WITH ITS EXTERNAL SLING
Abstract
The results of the helicopter dynamics research after the discharge of cargo transported on the external sling. These results allows to specify the limits of safe modes of transportation and to develop recommendations for actions in particular situations associated with discharge of the cargo are presented.
About the Authors
V. V. Efimov
МГТУ ГА
Russian Federation
Russian Federation
V. A. Ivchin
ОАО "МВЗ им. М.Л. Миля"
Russian Federation
Russian Federation
References
1. Rukovodstvo po letnoj jekspluatacii vertoleta Mi-8MTV [Flight operations manual of Mi8MTV helicopter]: vvedeno v dejstvie otdelom letnoj jekspluatacii Departamenta vozdushnogo transporta Ministerstva transporta Rossijskoj Federacii 14 maja 1994. (In Russian)
2. Efimov V.V., Parshencev 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. Scientific Bulletin MSTUCA] Nauchnyj vestnik MGTU GA. Moscow. 2008. no. 125. PP. 151 158. (In Russian)
3. Efimov V.V. Dinamicheskaja ustojchivost' gruza na trosovoj vneshnej podveske vertoleta [Investigation of the dynamic stability of cargo on the helicopter external sling. All-Russian magazine Flight], Obshherossijskij nauchno-tehnicheskij zhurnal "Polet", 2011, no. 3, PP. 26 32.
4. Efimov V.V. Avtokolebanija gruzov na trosovoj vneshnej podveske vertoleta [Autooscillations of cargo on the helicopter external sling. All-Russian magazine Flight], Obshherossijskij nauchno-tehnicheskij zhurnal "Polet", 2011, no. 12, PP. 23 28.
5. Volodko A.M. Vertolet v uslozhnennyh uslovijah jekspluatacii: uchebno-metodicheskoe posobie [Helicopter under extreme conditions: methodical manual], Moscow, KDU, 2007, 232 p. (In Russian)
6. Efimov V.V. Issledovanie avtokolebanij vertoleta s gruzom na vneshnej trosovoj podveske [Investigation of self-oscillations helicopter with the cargo on the external sling. Scientific Bulletin MSTUCA], Nauchnyj vestnik MGTU GA, Moscow, 2012, no. 177, PP. 65 – 71. (In Russian)
7. Ivchin V.A. Sovremennaja matematicheskaja model' dlja issledovanija dinamiki vertoleta na pilotazhnyh stendah [Modern mathematical model of the helicopter dynamics for simulators. Scientific Bulletin MSTUCA], Nauchnyj vestnik MGTU GA, Moscow, 2008, no 125, Serija "Ajeromehanika i prochnost'", PP. 54 – 62. (In Russian)
8. Efimov V.V. Matematicheskoe opisanie dvizhenija gruza na vneshnej podveske vertoleta [The mathematical description of the cargo motion on the helicopter external sling. Scientific Bulletin MSTUCA], Nauchnyj vestnik MGTU GA, Moscow, 2007, no. 111, Serija "Ajeromehanika i prochnost'", PP. 121 – 128. (In Russian)
9. Bisgaard M., Bendtsen J.D., La Cour-Harbo A. Modelling of Generic Slung Load System. Journal of Guidance, Control, and Dynamics, 2009, March, vol. 32, no. 2, PP. 573 585.
10. Cicolani L.S. and Kanning G. Equations of Motion of Slung-Load Systems, Including Multilift Systems, NASA, 1992, NASA-TP-3280, 132 p.
11. Stuckey R.A. Mathematical Modelling of Helicopter Slung-Load Systems, Air Operations Division Aeronautical and Maritime Research Laboratory, DSTO-TR-1257, 2001, 95 p.
12. Efimov V.V. O vlijanii gruza na vneshnej podveske vertoleta na ego ravnovesie [Effect of cargo on external sling helicopter on its equilibrium. Scientific Bulletin MSTUCA], Nauchnyj vestnik MGTU GA, Moscow, 2010, no. 154 (4), PP. 79 85. (In Russian)
13. 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. Scientific Bulletin MSTUCA] Nauchnyj vestnik MGTU GA, Moscow, 2010, no. 151 (1), PP. 130 137.
Review
For citations:
Efimov V.V., Ivchin V.A. THE RESULTS OF HELICOPTER DYNAMICS MATHEMATICAL MODELING AFTER DISCHARGE OF CARGO WITH ITS EXTERNAL SLING. Civil Aviation High Technologies. 2016;(223):101-108. (In Russ.)
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