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With the wide application of UAVs in military and civil fields, UAVs onboard photoelectric pod has gradually become one of the important supporting equipment of uAVs. The photoelectric pod can provide the UAV with real-time surveillance, reconnaissance, target recognition and other functions. This paper introduces the design and implementation of photoelectric pod on UAV.

Photoelectric pod is one of the important equipment of UAV, which can provide real-time target detection, monitoring and identification for UAV. In flight, the photoelectric pod will be affected by the complex aerodynamic environment and flight load, so the stability control of the photoelectric pod is the key to realize its function and performance.

Photoelectric pod is one of the essential components of modern weapons. It can obtain accurate image information in real time in complex environment, which helps commanders to judge the battle situation quickly, so as to formulate more effective attack strategy. However, in the process of high-speed flight, the photoelectric pod will be subjected to strong airflow, which will lead to uneven temperature distribution inside and outside the pod, resulting in a certain heat flow field. In order to better understand the characteristics of heat flow field inside the photoelectric pod, it is necessary to design a set of data acquisition system to obtain key parameters such as temperature and airflow velocity inside the pod. This paper will introduce the design of this data acquisition system.