This paper discusses a precision attitude and control technique for meeting these requirements utilizing a similar architecture that was adopted for the Laboratory of Atmospheric and Space Physics (LASP) SNOE (Student Nitrous Oxide Explorer) spinning spacecraft; SNOE has been operating with its ADCS architecture in low earth orbit (LEO) for over two years.
Precision ADCS of a spinning spacecraft for the Mars Aeronomy Explorer Mission
96th AIAA Aerospace Control and Guidance Systems Committee Meeting ; 2005 ; Hilton Head, SC, United States
2005-10-19
Conference paper
No indication
English
Mars Aeronomy Explorer (MAX): Study Employing Distributed Micro-Spacecraft
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