Flight Control Design for a Tailless Aircraft Using Eigenstructure Assignment

Table 2

SVD of lateral control distribution matrix^a.

Left singular vectors 𝑈stab					Singular values
0.0003	−0.0134	0.9999	0.0000	𝛽	0.1248
−0.0000	−0.0000	−0.0000	1.0000	𝜙	0.0279
0.9800	0.1992	0.0024	0.0000	𝑝𝑠	0.0000
−0.1992	0.9799	0.0132	0.0000	𝑟s	0.0000

^aAfter transformation to stability axis, no weights.