Towards a standard design model for quad-rotors: A review of current models, their accuracy and a novel simplified model

Luis Amezquita-Brooks, Eduardo Liceaga-Castro, Mario Gonzalez-Sanchez, Octavio Garcia-Salazar, Daniel Martinez-Vazquez

Producción científica: Contribución a una revistaArtículo de revisiónrevisión exhaustiva

31 Citas (Scopus)

Resumen

Applications based on quad-rotor-vehicles (QRV) are becoming increasingly wide-spread. Many of these applications require accurate mathematical representations for control design, simulation and estimation. However, there is no consensus on a standardized model for these purposes. In this article a review of the most common elements included in QRV models reported in the literature is presented. This survey shows that some elements are recurrent for typical non-aerobatic QRV applications; in particular, for control design and high-performance simulation. By synthesising the common features of the reviewed models a standard generic model SGM is proposed. The SGM is cast as a typical state-space model without memory-less transformations, a structure which is useful for simulation and controller design. The survey also shows that many QRV applications use simplified representations, which may be considered simplifications of the SGM here proposed. In order to assess the effectiveness of the simplified models, a comprehensive comparison based on digital simulations is presented. With this comparison, it is possible to determine the accuracy of each model under particular operating ranges. Such information is useful for the selection of a model according to a particular application. In addition to the models found in the literature, in this article a novel simplified model is derived. The main characteristics of this model are that its inner dynamics are linear, it has low complexity and it has a high level of accuracy in all the studied operating ranges, a characteristic found only in more complex representations. To complement the article the main elements of the SGM are evaluated with the aid of experimental data and the computational complexity of all surveyed models is briefly analysed. Finally, the article presents a discussion on how the structural characteristics of the models are useful to suggest particular QRV control structures.

Idioma originalInglés
Páginas (desde-hasta)1-23
Número de páginas23
PublicaciónProgress in Aerospace Sciences
Volumen95
DOI
EstadoPublicada - nov. 2017
Publicado de forma externa

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