Large-Scale Space-Based Solar Power Station: Packaging, Deployment and Stabilization of Lightweight Structures
US-2016376037-A1 · Dec 29, 2016 · US
US9199746B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9199746-B2 |
| Application number | US-201013321086-A |
| Country | US |
| Kind code | B2 |
| Filing date | May 19, 2010 |
| Priority date | May 19, 2009 |
| Publication date | Dec 1, 2015 |
| Grant date | Dec 1, 2015 |
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Various embodiments of the present invention include an attitude control system for use with small satellites. According to various embodiments, the system allows rapid retargeting (e.g., high slew rates) and full three-axis attitude control of small satellites using a compact actuation system. In certain embodiments, the compact actuation system includes a plurality of single-gimbaled control moment gyroscopes (SGCMG) arranged in a pyramidal configuration that are disposed within a small satellite.
Opening claim text (preview).
That which is claimed: 1. An attitude control system (ACS) for use with a pico- or a nano-satellite comprising: a plurality of single-gimbaled control moment gyroscopes (SGCMGs) arranged in a pyramidal configuration and operable to provide three-axis attitude control of the satellite, wherein each SGCMG defines a longitudinal axis with a first end and a second end, wherein the longitudinal axis of each SGCMG aligns with a respective side of the pyramidal configuration, and wherein…
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