Bifurcation Flight Dynamic Analysis of a Strake-Wing Micro Aerial Vehicle
Authors:
- Krzysztof Sibilski,
- Anna Sibilska-Mroziewicz,
- Andrzej Żyluk,
- Mirosław Nowakowski
Abstract
Non-linear phenomena are particularly important in -flight dynamics of micro-class unmanned aerial vehicles. Susceptibility to atmospheric turbulence and high manoeuvrability of such aircraft under critical flight conditions cover non-linear aerodynamics and inertia coupling. The theory of dynamical systems provides methodology for studying systems of non-linear ordinary differential equations. The bifurcation theory forms part of this theory and deals with stability changes leading to qualitatively different system responses. These changes are called bifurcations. There is a number of papers, the authors of which applied the bifurcation theory for analysing aircraft flight dynamics. This article analyses the dynamics of critical micro aerial vehicle flight regimes. The flight dynamics under such conditions is highly non-linear, therefore the bifurcation theory can be applied in the course of the analysis. The application of the theory of dynamical systems enabled predicting the nature of micro aerial vehicle motion instability caused by bifurcations and analysing the postbifurcation microdrone motion. This article presents the application of bifurcation analysis, complemented with time-domain simulations, to understand the open-loop dynamics of strake-wing micro aerial vehicle model by identifying the attractors of the dynamic system that manages upset behaviour. A number of factors have been identified to cause potential critical states, including nonoscillating spirals and oscillatory spins. The analysis shows that these spirals and spins are connected in a one-parameter space and that due to improper operation of the autopilot on the spiral, it is possible to enter the oscillatory spin.
- Record ID
- WUT37e9f913582e4f48a81c614bb6b22e0e
- Author
- Journal series
- Applied Sciences-Basel, ISSN 2076-3417, Monthly
- Issue year
- 2021
- Vol
- 11(4)
- No
- 1524
- Pages
- 1-23
- Publication size in sheets
- 1.10
- Keywords in English
- nonlinear dynamics of flight; bifurcation theory; micro aerial vehicles; strake-wing micro drones
- Keywords in original language
- nonlinear dynamics of flight; bifurcation theory; micro aerial vehicles; strake-wing micro drones
- ASJC Classification
- ; ; ; ; ;
- Abstract in original language
- Non-linear phenomena are particularly important in -flight dynamics of micro-class unmanned aerial vehicles. Susceptibility to atmospheric turbulence and high manoeuvrability of such aircraft under critical flight conditions cover non-linear aerodynamics and inertia coupling. The theory of dynamical systems provides methodology for studying systems of non-linear ordinary differential equations. The bifurcation theory forms part of this theory and deals with stability changes leading to qualitatively different system responses. These changes are called bifurcations. There is a number of papers, the authors of which applied the bifurcation theory for analysing aircraft flight dynamics. This article analyses the dynamics of critical micro aerial vehicle flight regimes. The flight dynamics under such conditions is highly non-linear, therefore the bifurcation theory can be applied in the course of the analysis. The application of the theory of dynamical systems enabled predicting the nature of micro aerial vehicle motion instability caused by bifurcations and analysing the postbifurcation microdrone motion. This article presents the application of bifurcation analysis, complemented with time-domain simulations, to understand the open-loop dynamics of strake-wing micro aerial vehicle model by identifying the attractors of the dynamic system that manages upset behaviour. A number of factors have been identified to cause potential critical states, including nonoscillating spirals and oscillatory spins. The analysis shows that these spirals and spins are connected in a one-parameter space and that due to improper operation of the autopilot on the spiral, it is possible to enter the oscillatory spin.
- DOI
- DOI:10.3390/app11041524 Opening in a new tab
- URL
- https://www.mdpi.com/2076-3417/11/4/1524 Opening in a new tab
- Language
- (en) English
- License
- File
-
- File: 1
- Bifurcation Flight Dynamic Analysis of a Strake-Wing Micro Aerial Vehicle, File WUT37e9f913582e4f48a81c614bb6b22e0e.pdf / 10 MB
- WUT37e9f913582e4f48a81c614bb6b22e0e.pdf
- publication date: 30-03-2022
- Bifurcation Flight Dynamic Analysis of a Strake-Wing Micro Aerial Vehicle, File WUT37e9f913582e4f48a81c614bb6b22e0e.pdf / 10 MB
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- Score (nominal)
- 100
- Score source
- journalList
- Score
- = 100.0, 24-05-2022, ArticleFromJournal
- Publication indicators
- = 0; = 0; : 2018 = 0.985; : 2018 (2 years) = 2.217 - 2018 (5 years) =2.287
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- Uniform Resource Identifier
- https://repo.pw.edu.pl/info/article/WUT37e9f913582e4f48a81c614bb6b22e0e/
- URN
urn:pw-repo:WUT37e9f913582e4f48a81c614bb6b22e0e
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