Efficient Method of Firing Angle Calculation for Multiple Launch Rocket System Based on Polynomial Response Surface and Kriging Metamodels

Table 2

Influencing factors and their variation ranges.

Factors	Units	Lower bound	Upper bound
B0	°	0.00	70.00
H0	m	0.00	5000.00
AT	mil	0.00	6400.00
RG	km	80.00	300.00
HT	m	0.00	5000.00
Ts	°C	-45.00	55.00