An Approximate Optimal Maximum Range Guidance Scheme for Subsonic Unpowered Gliding Vehicles

Table 6

Simulation results with atmospheric variations.

Scenario	(km)	(m/s)	Atmospheric variation	Terminal (km)	Proposed		Optimal		Error (%)
					Range		Range
					(km)	(km)	(km)	(km)
9	9.0	175.0	+5%	3.77	51.62	7.60	52.12	7.68	0.96
10	9.0	175.0	+10%	3.73	51.81	7.59	52.37	7.67	1.10
11	9.0	175.0	−5%	3.85	51.00	7.60	51.61	7.69	1.18
12	9.0	175.0	−10%	3.89	50.67	7.60	51.35	7.70	1.32