A Midcourse Guidance Method Combined with Trajectory Prediction for Antinear-Space-Gliding Vehicles

Table 2

Simulated comparison of the results for an interception of the maneuver target under multiple guidance methods.

Guidance methods	(-)	(-)	(°)	(m/s)
PN with TP	-0.0505	0.1326	20.0325	50.0214
PN without TP	-0.0121	-0.0327	-12.6711	19.0337
ZEM/ZEV ()	-0.0003	-9.286e-5	0.011	0.2371
ZEM/ZEV ()	0.0002	8.982e-5	0.005	0.3249
ZEM/ZEV ()	0.0007		-0.002	0.2495