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

Table 2

Stability and control derivatives uncertainty range knots (from [33]).

Parameter	Maximum	Minimum	Central value	Half range
𝐶𝑚𝑞	−4.3720	−16.1064	−10.2398	5.8666
𝐶𝑚𝛿𝑒	−0.7572	−1.2289	−0.9930	0.2359
𝐶𝑙𝛽	−0.0220	−0.0314	−0.0267	0.0047
𝐶𝑛𝑟	−0.1156	−0.2890	−0.2023	0.0867
𝐶𝑛𝛿𝑟	−0.0996	−0.1404	−0.1200	0.0204