School of Electronics and Information, Northwestern Polytechnical University, Xi'an 710129, China.
Aerospace Information Research Institute, Chinese Academy of Sciences, Beijing 100190, China.
Sensors (Basel). 2023 Apr 30;23(9):4421. doi: 10.3390/s23094421.
Environmental stability technology plays an important role in improving the adaptive range, image resolution and ensuring the stability of geometric parameters of aerial mapping camera. Traditional environmental stability methods directly implement active and passive thermal design to optical systems, which is easy to lead to radial temperature difference of optical components, and cannot eliminate the influence of pressure change. To solve the above problem, a method of environment stability design based on multi-dimensional structure is proposed. Firstly, the aerial mapping camera is designed as imaging system component (core) and sealing cylinder (periphery), and a sealed air insulation sandwich is formed between the two parts to realize the sealing design. A thermal interface is reserved outside the seal to avoid the radial thermal stress caused by direct heating of the optical parts, and a multi-dimensional Environmental stability structure is formed. Secondly, the core and the external thermal environment of aerial mapping camera in complex aviation environment are modeled and theoretically analyzed. Finally, the effectiveness and stability of the multi-dimensional structure method is verified by the thermal simulation and the flight. The results show that the thermal control power is 240 W, the thermal gradient of the optical system is less than 5 °C, the radial temperature difference is less than 0.5 °C. High quality image and ground measurement accuracy are obtained. Compared with tradition thermal control methods, the proposed method has the advantages of accuracy and low power consumption, which can effectively reduce the power consumption and difficulty of the thermal control.
环境稳定技术在提高航空测绘相机的适应范围、图像分辨率和保证几何参数稳定性方面起着重要作用。传统的环境稳定方法直接对光学系统进行主动和被动热设计,容易导致光学元件的径向温差,并且不能消除压力变化的影响。为了解决上述问题,提出了一种基于多维结构的环境稳定设计方法。首先,将航空测绘相机设计为成像系统组件(核心)和密封缸(外围),在两部分之间形成密封空气隔热夹层,实现密封设计。在密封外保留热接口,以避免光学部件直接加热引起的径向热应力,并形成多维环境稳定结构。其次,对复杂航空环境中航空测绘相机的核心和外部热环境进行建模和理论分析。最后,通过热模拟和飞行试验验证了多维结构方法的有效性和稳定性。结果表明,热控功率为 240W,光学系统的热梯度小于 5°C,径向温差小于 0.5°C。获得了高质量的图像和地面测量精度。与传统的热控方法相比,所提出的方法具有精度高、功耗低的优点,可有效降低热控的功耗和难度。