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

Table 3

Initial conditions and obtained maximum range using the proposed guidance scheme and optimal method.

Scenario	(km)	(m/s)	(km)	Initial	Proposed		Optimal		Error (%)
					(km)		(km)
1	9.0	175	10.56	0	51.33	7.60	51.84	7.68	0.98
2	8.0	224	10.56	5826	50.89	7.54	51.34	7.61	0.87
3	10.0	290	14.29	10392	78.18	7.46	79.08	7.54	1.14
4	6.0	299	10.56	22320	44.78	6.63	45.39	6.72	1.3
5	10.0	105	10.56	−4618	49.85	7.39	50.68	7.51	1.63
6	8.0	140	9.00	−2171	38.78	7.47	39.32	7.58	1.38