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

Table 1

AAA stability and control derivatives for 70 knots (from [33]).

Parameter	Value	Units
𝐶𝐷0	0.0513	[—]
𝐶𝐷𝛼	0.0863	[1/rad]
𝐶𝐷𝛿𝑒	0	[1/rad]
𝐶𝐷̇𝛼	0	[1/rad]
𝐶𝐷𝑞	0	[1/rad]
𝐶𝐷𝑢	0.0011	[1/rad]
𝐶𝐿0	0	[—]
𝐶𝐿𝛼	4.5465	[1/rad]
𝐶𝐿𝛿𝑒	0.3792	[1/rad]
𝐶𝐿̇𝛼	1.8918	[1/rad]
𝐶𝐿𝑞	5.5046	[1/rad]
𝐶𝐿𝑢	0.0017	[1/rad]
𝐶𝑚0	0.0020	[—]
𝐶𝑚𝛼	−0.3937	[1/rad]
𝐶𝑚𝛿𝑒	−0.8778	[1/rad]
𝐶𝑚̇𝛼	−4.3787	[1/rad]
𝐶𝑚𝑞	−8.0532	[1/rad]
𝐶𝑚𝑢	0.0002	[1/rad]
𝐶𝑦𝛽	−0.3602	[1/rad]
𝐶𝑦̇𝛽	0	[1/rad]
𝐶𝑦𝑝	0.0085	[1/rad]
𝐶𝑦𝑟	0.2507	[1/rad]
𝐶𝑦𝛿𝑎	0	[1/rad]
𝐶𝑦𝛿𝑟	0.1929	[1/rad]
𝐶𝑙𝛽	−0.0266	[1/rad]
𝐶𝑙̇𝛽	0	[1/rad]
𝐶𝑙𝑝	−0.3819	[1/rad]
𝐶𝑙𝑟	0.0514	[1/rad]
𝐶𝑙𝛿𝑎	0.3490	[1/rad]
𝐶𝑙𝛿𝑟	0.0154	[1/rad]
𝐶𝑛𝛽	0.1022	[1/rad]
𝐶𝑛̇𝛽	0	[1/rad]
𝐶𝑛𝑝	−0.0173	[1/rad]
𝐶𝑛𝑟	−0.1270	[1/rad]
𝐶𝑛𝛿𝑎	−0.0088	[1/rad]
𝐶𝑛𝛿𝑟	−0.0996	[1/rad]