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

Figure 7

Changes in the flight parameters for interception using different midcourse guidance methods under multiple constraints based on predictions of the trajectory. (a) Normal overload change curve. (b) Lateral overload change curve. (c) Curve of the track angle curve. (d) Curve of the track declination angle. (e) Relative distance curve. (f) Velocity curve.

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