Research Article
LMI-Based Robust Stabilization of a Class of Input-Constrained Uncertain Nonlinear Systems with Application to a Helicopter Model
Table 3
Numerical simulation results using Theorem 3 for different values of the parameter
λ and for
and
.
| | | | | | | |
| | | | | | | | m | 0.01327 | 0.013319 | 0.013316 | 0.013320 | 0.013321 | 0.013321 | | 0.0321 | 0.8835 | 1.2411 | 2.4613 | 6.8305 | 9.3191 | | 0.1500 | 3.6262 | 3.6585 | 3.4313 | 3.3309 | 3.3217 | | 9.9995 | 14.5636 | 14.3332 | 14.3665 | 14.4657 | 14.7111 | | 0.0360 | 2.1881 | 4.8950 | 6.0531 | 6.2291 | 6.1668 | γ | 9990.7 | 997.292 | 99.0173 | 9.8937 | 0.9851 | 0.4922 |
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