Flight Control Design for a Tailless Aircraft Using Eigenstructure Assignment

Table 7

Longitudinal gain/phase margins^a.

	Gain margin	Phase margin	Frequency
	(db)	(deg)	(r/s)
𝛿pf	±14.68	±69.09	7.87
𝛿ptv	±26.02	±84.28	9.95
𝑐^∗	±28.92	±85.90	17.08
𝛼	±5.33	±33.15	0.0085
𝑞	±29.22	±86.04	17.44
∫𝑐^∗	±4.81	±30.23	0.0097

^aGain and phase margins use model with actuator dynamics.