Optimization of Trajectory Correction Scheme for Guided Mortar Projectiles

Table 1

Initial conditions for example simulation.

State	Unit	Unperturbed value	Perturbed value
launching elevation angle	deg	78.86	78.26
Launching azimuth angle	deg	−0.13	0.80
Initial velocity	m/s	280	285
Wind	m/s	0	3
Wind direction	deg	0	135