Adaptive and Resilient Flight Control System for a Small Unmanned Aerial System

Table 3

Closed-loop infinity norm associated to each uncertainty.

Parameter	‖𝐅𝐥(𝐏^𝟏,𝐊^𝟏)‖∞
𝐶𝑚𝑞	0.3846
𝐶𝑚𝛿𝑒	0.2451
𝐶𝑙𝛽	0.0100
𝐶𝑛𝑟	0.3816
𝐶𝑛𝛿𝑟	0.1674
All	0.5617