Table 1. Main parameters and values of launch vehicle [9]: S.I.(specific impulse), L.C.(lift coefficient)

Parameter	Initial value	Parameter	Initial value	Parameter	Initial value
S.I. (θ1)	255 N-sec/kg	L.C. (θ2)	3.5	Pitch (θ3)	85 deg
Yaw (θ4)	120 deg	Latitude (θ5)	31.251 deg	Longitude (θ6)	131.08 deg
Altitude (θ7)	194 m	Mass (θ8)	45,247.4 kg	Thrust force (θ9)	1,147,000 N