Development and validation of the multicopter modelling code: a physics-based tool for multicopter analysis

被引:1
作者
Oppong, David Kofi [1 ]
Obu, Evans [2 ]
Asare, Timothy [3 ]
Aidam, God'sable Sitsofe Koku [1 ]
机构
[1] Kwame Nkrumah Univ Sci & Technol, Dept Mech Engn, Kumasi, Ghana
[2] Christian Serv Univ Coll, Dept Comp Sci & Informat Technol, Kumasi, Ghana
[3] Ashesi Univ, Dept Engn, Accra, Ghana
关键词
Multicopter; Model; MATLAB; Physics;
D O I
10.1108/AEAT-01-2022-0011
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Purpose This study aims to present details of the development and validation of the multicopter modelling code (MMC), a tool for the analysis of small-scale multicopters based on flight physics. Design/methodology/approach The development effort involved the study of aircraft dynamics and translating the equations of motion into MATLAB code. The authors also developed several auxiliary functions, so that the tool could trim the aircraft about a steady state, linearize the dynamic equations to produce a model that could be used for control systems design and carry out flight simulation. Findings MMC proved to be of good accuracy, producing results similar to those of other software such as AcuSolve, Overflow and the Rensselaer Multicopter Analysis Code (RMAC), which served as the motivation for this study. Originality/value The tool presented here provides an alternative to the aforementioned software, which are not freely available, programmed in MATLAB, a language well known to engineers and scientists.
引用
收藏
页码:1684 / 1691
页数:8
相关论文
共 19 条
[1]  
Groves PD, 2008, ARTECH HSE GNSS TECH, P3
[2]  
Jenie Y.I., 2020, MATH MODELLING SIMUL
[3]  
Kaminski D.A., 2005, Introduction to Thermal and Fluids Engineering
[4]  
Kotarski D., 2016, Int. J. Theor. Appl. Mech, V1, P233
[5]  
Leishman J. G., 2006, Principles of Helicopter Aerodynamics
[6]   Computational Study on Rotor Interactional Effects for a Quadcopter in Edgewise Flight [J].
Misiorowski, Matthew ;
Gandhi, Farhan ;
Oberai, Assad A. .
AIAA JOURNAL, 2019, 57 (12) :5309-5319
[7]  
Niemiec, 2019, DEV VALIDATION RENSS, P1
[8]  
Niemiec, COMP QUADROTOR FLIGH
[9]  
Niemiec R., 2017, EFFECT ELASTIC BLADE
[10]  
Niemiec R., 2016, 72 ANN FORUM AM HELI