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High-Accuracy Self-Calibration for Smart Optical Orbiting Payloads Integrated with Attitude and Position Determination

机译:集成了姿态和位置确定功能的智能光学轨道有效载荷的高精度自校准

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摘要

A high-accuracy space smart payload integrated with attitude and position (SSPIAP) is a new type of optical remote sensor that can autonomously complete image positioning. Inner orientation parameters (IOPs) are a prerequisite for image position determination of an SSPIAP. The calibration of IOPs significantly influences the precision of image position determination of SSPIAPs. IOPs can be precisely measured and calibrated in a laboratory. However, they may drift to a significant degree because of vibrations during complicated launches and on-orbit functioning. Therefore, laboratory calibration methods are not suitable for on-orbit functioning. We propose an on-orbit self-calibration method for SSPIAPs. Our method is based on an auto-collimating dichroic filter combined with a micro-electro-mechanical system (MEMS) point-source focal plane. A MEMS procedure is used to manufacture a light transceiver focal plane, which integrates with point light sources and a complementary metal oxide semiconductor (CMOS) sensor. A dichroic filter is used to fabricate an auto-collimation light reflection element. The dichroic filter and the MEMS point light sources focal plane are integrated into an SSPIAP so it can perform integrated self-calibration. Experiments show that our method can achieve micrometer-level precision, which is good enough to complete real-time calibration without temporal or spatial limitations.
机译:集成了姿态和位置(SSPIAP)的高精度太空智能有效载荷是一种新型的光学遥感器,可以自动完成图像定位。内部方向参数(IOP)是确定SSPIAP的图像位置的先决条件。 IOP的校准会显着影响SSPIAP图像位置确定的精度。可以在实验室中精确测量和校准IOP。但是,由于复杂的发射和在轨运行过程中的振动,它们可能会漂移很大。因此,实验室校准方法不适合在轨运行。我们提出了一种针对SSPIAP的在轨自校准方法。我们的方法基于自动准直二向色滤光片与微机电系统(MEMS)点源焦平面的组合。 MEMS程序用于制造光收发器焦平面,该光收发器焦平面与点光源和互补金属氧化物半导体(CMOS)传感器集成在一起。二向色滤光片用于制造自准直光反射元件。二向色滤光片和MEMS点光源焦平面集成到SSPIAP中,因此它可以执行集成的自校准。实验表明,我们的方法可以达到微米级的精度,足以在没有时间或空间限制的情况下完成实时校准。

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