Simultaneous quadrotor autopilot system and collective morphing system design

被引:55
作者
Kose, Oguz [1 ]
Oktay, Tugrul [2 ]
机构
[1] Gumushane Univ, Dept Comp Technol, Kelkit Aydin Dogan Vocat Sch, Gumushane, Turkey
[2] Erciyes Univ, Dept Aeronaut Engn, Fac Aeronaut & Astronaut, Kayseri, Turkey
关键词
Optimization; UAVs; Quadrotor; Modelling; PID; Collective morphing; SPSA; APPROXIMATION; HELICOPTER;
D O I
10.1108/AEAT-01-2020-0026
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Purpose The purpose of this paper is to design a quadrotor with collective morphing using the simultaneous perturbation stochastic approximation (SPSA) optimization algorithm. Design/methodology/approach Quadrotor design is made by using Solidworks drawing program and some mathematical performance relations. Modelling and simulation are performed in Matlab/Simulink program by using the state space model approaches with the parameters mostly taken from Solidworks. Proportional integral derivative (PID) approach is used as control technique. Morphing amount and the best PID coefficients are determined by using SPSA algorithm. Findings By using SPSA algorithm, the amount of morphing and the best PID coefficients are determined, and the quadrotor longitudinal and lateral flights are made most stable via morphing. Research limitations/implications It takes quite a long time to model the quadrotor in Solidworks and Matlab/Simulink with the state space model and using the SPSA algorithm. However, this situation is overcome with the proposed model. Practical implications Optimization with SPSA is very useful in determining the amount of morphing and PID coefficients for quadrotors. Social implications SPSA optimization method is useful in terms of cost, time and practicality. Originality/value It is released to improve performance with morphing, to determine morphing rate with SPSA algorithm and to determine PID coefficients accordingly.
引用
收藏
页码:1093 / 1100
页数:8
相关论文
共 29 条
  • [1] [Anonymous], 2007, DESIGN CONTROL QUADR
  • [2] [Anonymous], 2007, P AIAA GUID NAV CONT, DOI DOI 10.2514/6.2007-6461
  • [3] [Anonymous], 2011, UNMANNED AIRCRAFT SY
  • [4] Avant T., 2018, 2018 ANN AM CONTR C
  • [5] Bai Y., 2017, Control and Simulation of Morphing Quadcopter
  • [6] Modeling and control of a quadrotor with variable geometry arms
    Barbaraci, Gabriele
    [J]. JOURNAL OF UNMANNED VEHICLE SYSTEMS, 2015, 3 (02) : 35 - 57
  • [7] Bhatnagar S., 2013, Stochastic Recursive Algorithms for Optimization
  • [8] Bresciani T., 2008, MODELLING IDENTIFICA, V0280-5316
  • [9] Celik H., 2016, J AERONAUTICS SPACE, V9
  • [10] Desbiez A., 2017, 2017 WORKSH RES ED D