A method for observing the condensation along the meridian of the earth

By employing a deceleration-based fixed-scan observation method along Earth's meridians and a high-stability algorithm, the problems of motion ambiguity and target identification difficulties in satellite observations along Earth's meridians were solved, achieving high-quality imaging and continuous optimization of observations, and meeting the high-stability requirements.

CN122402811APending Publication Date: 2026-07-17INNOVATION ACAD FOR MICROSATELLITES OF CAS +1

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
INNOVATION ACAD FOR MICROSATELLITES OF CAS
Filing Date
2026-03-11
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

Existing technologies struggle to effectively reduce satellite speed relative to the ground through attitude maneuvers, hindering high-quality imaging and continuous optimization of observations. This is particularly true during observations along Earth's meridians, where motion blur and target identification remain problematic.

Method used

The method of decelerating fixed-scan observation along the Earth's meridian is adopted. By uploading fixed-scan parameter configuration commands and combining them with a high-stability algorithm, the satellite's autonomous three-axis attitude angles and angular velocities are calculated. The process is divided into two stages: advance maneuver and fixed-scan observation. This ensures that the observation area is evenly divided in each attitude control cycle. High-precision double-precision floating-point storage and arcsine formula are used to calculate attitude angles and eliminate attitude angular velocity jitter.

Benefits of technology

It achieved highly stable satellite observations along the Earth's meridian, eliminated attitude and angular velocity jitter, met high stability requirements, improved imaging quality and target recognition capabilities, and adapted to diverse mission needs.

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Abstract

本发明公开了一种沿地球经线进行降速凝扫观测的方法,通过上注的凝扫参数计算卫星姿态,分为提前机动及凝扫两个环节;提前机动环节基于上注的凝扫参数设置指令中的凝扫开始时刻,以及提前机动时间,在时刻基于卫星位置速度提前指向初始凝扫目标点;凝扫环节在时刻开始利用凝扫时长将凝扫区域进行均匀划分,保证每一姿控周期均有与之对应的地面目标区域,凝扫比例由地面进行规划;凝扫时长及凝扫区域由地面确定,凝扫区域纬度差不能超过15°,凝扫环节时长不能超过5min;算法最终输出为凝扫时长内时间序列对应的期望三轴姿态角及角速度。提出了一种沿地球经线进行降速凝扫观测的方法,并结合工程实际,利用高稳定度算法实现对目标的持续优化观测。
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