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Attitude reference generation for spacecraft with rotating solar arrays and pointing constraints

Riccardo Calaon Cody Allard Hanspeter Schaub

航天动力学（英文）2025，Vol.9Issue(3)：389-406,18.

航天动力学（英文）2025，Vol.9Issue(3)：389-406,18.DOI:10.1007/s42064-024-0245-1

Attitude reference generation for spacecraft with rotating solar arrays and pointing constraints

Riccardo Calaon ¹Cody Allard ²Hanspeter Schaub¹

作者信息

1. Ann and H.J.Smead Department of Aerospace Engineering Sciences,University of Colorado Boulder,Boulder,CO 80303,USA
2. Laboratory for Atmospheric and Space Physics,Boulder,CO 80303,USA
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摘要

关键词

spacecraft attitude guidance/optimal power generation/articulating solar arrays/pointing constraints

Key words

spacecraft attitude guidance/optimal power generation/articulating solar arrays/pointing constraints

引用本文复制引用

Riccardo Calaon,Cody Allard,Hanspeter Schaub..Attitude reference generation for spacecraft with rotating solar arrays and pointing constraints[J].航天动力学（英文）,2025,9(3):389-406,18.

基金项目

Support for this effort was provided by the Emirates Mission to the Asteroid Belt which is led by the UAE Space Agency in collaboration with the Laboratory for Atmospheric and Space Physics at the University of Colorado Boulder as its knowledge partner. （）

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