Multicriterial minimax method for designing fpv-type unmanned aerial vehicle based on morphological analysis and latent variable theory


Аuthors

Ananjev A. V.1*, Kuziyarov N. F.2, Moiseev S. I.3

1. Plekhanov Russian University of Economics, Voronezh, Russian Federation
2. MESC Air Force “Air Force Academy named after professor N.E. Zhukovskii and Yu.A. Gagarin” (branch in the city of Chelybinsk), 40, Gorodok-11, Chelybinsk, 454015, Russia
3. Voronezh State Technical University, VSTU, 14, Moskovsky prospect, Voronezh, 394026, Russia

*e-mail: Ananyev-Alexandr@yandex.ru

Abstract

The paper presents a multi-criteria minimax methodology for designing an unmanned aerial vehicle (UAV), based on morphological analysis and the theory of latent variables. An analysis of existing approaches to UAV design was conducted. Based on the analysis, it was proposed to identify the basic part of the technical device functional elements, the main characteristics of which should ensure key requirements, for example, for the mass of the payload. Morphological analysis is formalized by an algorithm that includes multi-criteria selection procedures based on the theory of latent variables. The algorithm for solving the problem of selecting a rational configuration for the UAV has been considered, through which a compromise solution has been obtained regarding the dilemma of «algorithm complexity» versus «solution quality» based on the use of a controlled parameter. A rational component selection algorithm for the basic configuration of the product is presented, to which non-basic components will be added later. The scheme of this algorithm and the evaluation of its properties have been implemented. A graph showing the dependence of the number of comparisons on the parameters of the type is presented, illustrating the complexity of the calculations. The allocation of basic part formation stage structure to achieve the minimum necessary requirements for the main indicator with subsequent maximization by a set of all functional units parameters involves the implementation of the “multi-criteria minimax” procedure. The multi-criteria minimax implementation allows for reasonable limitation of requirements and ensuring the minimum achievable UAV form factor. 

Keywords:

morphological analysis, latent variables, algorithm, design, mathematical modeling, configuration

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