Adaptive Backstepping Sliding Mode Control for Quadrotor UAV

Table 1

Physical parameters of quadrotor UAV.

Parameters	Numerical value	The physical meaning of parameter
	1.0	The mass of the quadrotor UAV ()
	9.8	Gravity acceleration ()
	0.005	The moment of inertias of the Y-axis ()
	0.005	The moment of inertias of the X-axis ()
	0.01	The moment of inertias of the Z-axis ()
	0.2	The length of the quadrotor UAV from the end of each rotor to the center of gravity ()
	0.00002	The moment of inertia of the motor rotor ()
	0.00003	The drag coefficient
	0.00000006	The lift coefficient