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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.

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This page is a summary of: Simultaneous quadrotor autopilot system and collective morphing system design, Aircraft Engineering and Aerospace Technology, June 2020, Emerald,
DOI: 10.1108/aeat-01-2020-0026.
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