JOURNAL ARTICLE

A note on application and analysis of the non-linear and non-ideal dynamic behavior of the Mathieu equation.

  • Published In: Mathematics in Engineering, Science & Aerospace (MESA), 2024, v. 15, n. 3. P. 801 1 of 3

  • Database: Academic Search Ultimate 2 of 3

  • Authored By: Ribeiro, Mauricio A.; Balthazar, Jose M.; Tusset, Angelo M.; Felix, Jorge L. P.; Daum, Hilson H.; Miranda, Sergio B. 3 of 3

Abstract

Cargo transport to the space station and the transport of satellites to orbit the Earth are necessary for not only scientific analysis, but also for the telecommunications sector; therefore, the use of rockets with propellant fuel has been growing. Therefore, our manuscript proposes a mathematical model to analyze nonlinear dynamic behavior. Such a model is based on Mathieu's solution. However, we consider that the application of force for rocket propulsion is not ideal. The formulation of the applied force is based on Bessel s equations and has a dependence on parameters (ao and bo) that enable interesting characteristics. such as ao = 0 which makes it possible to turn the non-ideal force into a force ideal, that is, a simple oscillatory force. And as a result. the parametric set was established to diagnose the chaotic and periodic behavior that can be observed in mathematical modeling. Establishing these analyzes allows the application of future work in the development of control projects to reduce vibrations that can cause anomalies in the trajectories for the system's entry into orbit. Another application of nonlinear dynamic analysis is to establish regions for future suppression of the chaotic regime that were observed in our numerical analyses. [ABSTRACT FROM AUTHOR]

Additional Information

  • Source:Mathematics in Engineering, Science & Aerospace (MESA). 2024/09, Vol. 15, Issue 3, p801
  • Document Type:Article
  • Subject Area:History
  • Publication Date:2024
  • ISSN:2041-3165
  • Accession Number:180439341
  • Copyright Statement:Copyright of Mathematics in Engineering, Science & Aerospace (MESA) is the property of Nonlinear Studies and its content may not be copied or emailed to multiple sites without the copyright holder's express written permission. Additionally, content may not be used with any artificial intelligence tools or machine learning technologies. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract. (Copyright applies to all Abstracts.)

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