Optimization of the PNG Law for a Dual-Spin Mortar with Fixed Canards

Table 4

Initial conditions for scheme 1.

State	Nominal	Perturbated
Launch elevation angle (degrees)	45.0	46.0
Launch azimuth angle (degrees)	0.0	0.0
Muzzle velocity (m/s)	341.0	338.0
Wind	0.0	9.0
Axial force coefficient multiplier	1.0	1.1