Robust Predictive Functional Control for Flight Vehicles Based on Nonlinear Disturbance Observer

Table 1

Coefficients of the flight vehicle model.

Coefficient	Value	Unit
		deg^−3
		deg^−2
		deg^−1
		deg^−1
		m^2
		s
		kg
		Kg⋅m^2
		deg^−3
		deg^−2
		deg^−1
		deg^−1
		m
		m/s^2
		m/s
		kg/m^3