Firing Control Optimization of Impulse Thrusters for Trajectory Correction Projectiles

Table 1

Initial conditions and disturbances.

Parameter	Unit	Mean value	Standard deviation
Launching elevation angle	deg	42.51	0.2
Launching azimuth angle	deg	0.1	0.2
Impulse of the main rocket motor	%	100	0.1
Wind	m/s	0	2