The attitude of high-atmospheric payloads is examined. A rocket-borne attitude measuring device was used and primary data was converted into Euler angles. For error detection in the Euler angle values, a consistence check based on an analysis of variation of the Euler angles in time was successfully applied on attitude data of nutating payloads.
Attitude Data Consistence Check of Rocket Payloads
1984
34 pages
Report
No indication
English
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