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

Figure 8

Comparison of results considering predictions of trajectories of NSGVs under PN and the proposed guidance methods. (a) Trajectories of interception using different midcourse guidance methods. (b) Trajectories of interception during terminal guidance phase using different midcourse guidance methods. (c) Normal overload change curve during terminal guidance phase. (d) Lateral overload change curve during terminal guidance phase.

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