LMI-Based Robust Stabilization of a Class of Input-Constrained Uncertain Nonlinear Systems with Application to a Helicopter Model

Table 2

Numerical simulation results using Theorem 3 for different values of the parameter λ and for and .

m	0.013275	0.013283	0.013268	0.013243	0.013251	0.013262
	0.0067	0.0181	0.7729	1.9138	5.4867	7.7133
	0.0800	0.1020	2.2687	2.6586	2.6496	2.6447
	0.0048	0.0029	0.0043	0.0011	0.0022	0.0038
	0.0112	0.0155	0.4577	0.7132	0.7459	0.7475
γ	99.1571	9.9099	0.9893	0.0986	0.0099	0.0049