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引用次数: 2

摘要

立方体卫星是一种纳米卫星系统标准,其中纳米卫星具有结构、动力、遥测、有效载荷以及其他子系统,然而,它适合1.3公斤和10cm×10cm×10cm模块[1]。纳米卫星在设计上具有灵活性;近年来,人们对如何实现子系统提出了一些建议。分辨率不断提高,这反过来又导致需要更高的指向精度。它们突破了小尺寸和低成本的限制,主要用于大学,这些卫星的尺寸在几十厘米左右,重量在1到10公斤之间,价格通常在数万美元。
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MEMS gyroscope for attitude propagation and determination for nanosatellites
Cubesat is a nano-satellite system standard, where a nano-satellite has structure, power, telemetry, payload among other subsystems, however, it fits up to 1.3 kilograms and 10cm×10cm×10cm modules [1]. Nano-satellites present flexibility in design; in recent years there are several proposals on how to implement the subsystems. The resolution continued to improve, which in turn lead to the need for higher accuracy pointing. They push the bounds of small size and low cost developed to provide cheap access to space and used primarily by universities, these satellites are measured in the tens of centimeters, weigh between one and ten kilograms, and usually cost in the tens of thousands of dollars.
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