Author Affiliations
1 Aeronautics Engineering College, Air Force Engineering University, Xi'an, Shaanxi 710038, China2 No. 95910 Troop, People's Liberation Army, Jiuquan, Gansu 735305, Chinashow less
Fig. 1. Relative position relationship between airborne detector and target
Fig. 2. Schematic of migration of feature space
Fig. 3. Dual-color-ratio-feature point distribution under maneuvering mode
Fig. 4. Migration process of feature space under maneuvering mode
Fig. 5. (a) Two-dimensional motion tracks of target and airborne detector; (b) target lateral overloading versus time; (c) target attitude angle versus time; (d) dual-color-ratio-feature versus target attitude angle and lateral overloading
Fig. 6. Dual-color-ratio-feature point distribution under quarter turn maneuver
Fig. 7. Gauss mixture distributions of dual-color-ratio-feature sub-space under different variations of target attitude angle. (a) Δα=50.34°; (b) Δα=36.16°; (c) Δα=14.23°; (d) Δα=3.52°
Fig. 8. Sequential dual-color-ratio-feature point distribution under linear motion
Fig. 9. Gauss mixture distributions of sequential dual-color-ratio-feature sub-space under linear motion. (a) Before adjacent feature sub-spaces merged; (b) after adjacent feature sub-spaces merged
Fig. 10. Sequential dual-color-ratio-feature point distribution under quarter turn maneuver
Fig. 11. Gauss mixture distributions of sequential dual-color-ratio-feature sub-space under quarter turn maneuver. (a) Before adjacent feature sub-spaces merged; (b) after adjacent feature sub-spaces merged
Fig. 12. Sequential dual-color-ratio-feature point distribution under circle maneuver
Fig. 13. Gauss mixture distribution of sequential dual-color-ratio-feature sub-space under circle maneuver
Maneuvering mode | Average recognition rate | Average time /s |
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Head-on linear maneuver | 0.99 | 0.077 | Rear-end linear maneuver | 1.00 | 0.075 | Head-on 90° angle turn | 0.87 | 0.070 | Rear-end 90° angle turn | 0.94 | 0.073 | Head-on snake maneuver | 0.96 | 0.081 | Rear-end snake maneuver | 0.95 | 0.082 | Circle maneuver | 0.96 | 0.082 | Head-on pull up | 0.88 | 0.071 | Head-on swoop down | 0.85 | 0.073 | “8-based” maneuver | 0.88 | 0.095 | Head-on 180° angle turn | 0.90 | 0.086 | Rear-end 180° angle turn | 0.91 | 0.087 |
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Table 1. Recognition rate of different maneuvering modes of point target