Spacecraft Angular Rates Estimation with Gyrowheel Based on Extended High Gain Observer

Author: Liu Xiaokun   Yao Yu   Ma Kemao   Zhao Hui   He Fenghua  

Publisher: MDPI

E-ISSN: 1424-8220|16|4|537-537

ISSN: 1424-8220

Source: Sensors, Vol.16, Iss.4, 2016-04, pp. : 537-537

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Abstract