Invention Grant
US08688296B2 Method for maximum data collection with a control moment gyroscope controlled satellite 有权
用控制时间陀螺仪控制的卫星进行最大数据收集的方法

Method for maximum data collection with a control moment gyroscope controlled satellite
Abstract:
The present invention relates to a method for maneuvering an imaging satellite, and more particularly a method for commanding control moment gyroscopes on an imaging satellite to change the attitude of the satellite. In one embodiment, a method for generating a gimbal rate trajectory for maneuvering a satellite to point to a target includes providing a final attitude for pointing to the target and a final satellite rate for imaging the target, providing an initial attitude and an initial set of gimbal angles, and determining a gimbal rate trajectory from the initial set of gimbal angles to a final set of gimbal angles.
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