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DETERMINE THE RANGE OF VARIATION OF THE CONTROL SUBSYSTEM OUTPUT PARAMETERS

Abstract

For the evaluation of the tolerance of output parameters of the controls functional subsystem the hydraulic system under different operating conditions and phases of flight are given mathematical relationships and the results obtained in Mathcad are given in graphical form.

About the Author

M. A. Bobrin
МГТУ ГА
Russian Federation


References

1. Goniodskiyj V.I., Sklyanskiyj F.I., Shumilov I.S. Privod rulevihkh poverkhnosteyj samoletov. M.: Mashinostroenie. 1974. 320 p. (In Russian).

2. Matvienko A.M., Zverev I.I. Proektirovanie gidravlicheskikh sistem letateljnihkh apparatov. M.: Mashinostroenie. 1982. 296 p. (In Russian).

3. Bobrin M.A., Klemina L.G., Kozlov A.N. Opredelenie jekspluatacionnogo diapazona izmenenija vyhodnyh parametrov funkcional'nyh podsistem gidravlicheskih sistem letatel'nyh apparatov. Nauchnihyj Vestnik MGTU GA. 2011. № 200. Pp. 16-19. (In Russian).


Review

For citations:


Bobrin M.A. DETERMINE THE RANGE OF VARIATION OF THE CONTROL SUBSYSTEM OUTPUT PARAMETERS. Civil Aviation High Technologies. 2015;(212):133-136. (In Russ.)

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