Guardian Map Approach to Feasible Range of Static Stability Margin of Hypersonic Flight Vehicles with Input Saturation

Table 2

Parameters of the HFV model.

No	Parameters	Symbols	Nominal values	Units
1	Fuselage length		100	ft
2	Axial distance of the CG from the leading edge		55	%
3	Reference area		17	ft^2
4	Mean aerodynamic chord (MAC)		17	ft
5	Shift distance of scramjet engine		8.36	ft
6	Static stability margin		-55.01	%
7	Stability derivatives		4.6773	rad^-1
8	Control derivatives		0.7622	rad^-1
9	Net control derivatives		-1.7090	rad^-1