Fig. 1. Schematic diagram of aircraft atmospheric disturbance field

Fig. 2. Atmospheric disturbance field formed during airplane flight

Fig. 3. Schematic diagram of background schlieren Technology

Fig. 4. Visualized results diagram of helicopter flow field

Fig. 5. Schematic diagram of plasma sheath

Fig. 6. Plasma sheath characteristics acquired by RAM project

Fig. 7. Schematic diagram of lidar detection

Fig. 8. Particle scattering and the generation of sky polarized light

Fig. 9. Theoretical model diagram of atmospheric polarization mode

Fig. 10. Schematic diagram of polarization detection system

Fig. 11. Aircraft wake diagram

Fig. 12. Schematic diagram of lidar detecting aircraft wake

Fig. 13. Schematic diagram of geomagnetic anomaly

Fig. 14. Schematic diagram of geomagnetic anomaly detection

Fig. 15. Aircraft atmospheric disturbance field imaging system and detection results

Fig. 16. Optimized detection results of aircraft atmospheric disturbance field

Fig. 17. Comparison of processing results between cross-correlation (left) and optical flow algorithm (right)

Fig. 18. Ca-K solar eclipse atmospheric disturbance field imaging system and detection results

Fig. 19. Interaction image of the atmospheric disturbance field of two aircraft

Fig. 20. X-band signal amplitude and phase jitter of the RAM-C flight test in the United States

Fig. 21. Image-based all-sky automatic test device and measurement results

Fig. 22. Wake detection experiment results

Fig. 23. Wake detection experiment results