DYNAMIC MODELLING OF MAV

The Newton-Euler method is used for formulating the non-linear dynamic model for the MAV and the formulated model is explained with aerodynamic forces and torques as well which are usually neglected in most of the typical works. 

The mathematical dynamic model of Six Degrees of Freedom (6-DOF) of an aircraft is nonlinear and it is linearized about a flight condition. Mathematical modelling of non-linear equations of motion is the first step of MAV design