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A New Method for Analyzing Aero-Optical Effects with Transient Simulation
Bo Yang1, Zichen Fan1, He Yu1
1School of Astronautics, Beihang University, Beijng 100191, China.
Sensors (Basel, Switzerland)
|April 3, 2021
Summary
This study introduces a new method to analyze aero-optical effects by focusing on micro-scale structures and photon energy scattering. This approach reveals micro-scale turbulence significantly impacts wavefront distortion, improving optical sensor accuracy.
Area of Science:
- Optics and Photonics
- Fluid Dynamics
- Aerospace Engineering
Background:
- Aero-optical effects, caused by airflow over high-speed aircraft, degrade optical sensor accuracy.
- Existing research primarily addresses light refraction from large-scale turbulent structures.
- The impact of micro-scale structures on aero-optical phenomena remains less understood.
Purpose of the Study:
- To propose and validate a novel method for analyzing aero-optical effects.
- To investigate the contribution of micro-scale structures to wavefront distortion.
- To develop a simulation tool for understanding and mitigating aero-optical effects.
Main Methods:
- Developed a method analyzing photon energy scattering from micro-scale structures.
- Quantitatively analyzed the propagation equation for wavefront distortion.
- Designed a transient simulator using scaling models and artificial vortex structures.
Main Results:
- Micro-scale structures can contribute significantly more to wavefront distortion than large-scale structures.
- Simulation results confirm that photon energy scattering from micro-scale structures accurately represents aero-optical phenomena.
- Demonstrated the application of the simulator in optimizing star sensor parameters for hypersonic vehicles.
Conclusions:
- Micro-scale structures are critical to understanding aero-optical effects.
- The proposed analysis method and simulator offer a new perspective for studying aero-optical phenomena.
- This research can lead to improved optical sensor performance on high-speed platforms.
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