Journal of Control Science and Engineering / 2013 / Article / Tab 4

Research Article

Design of Attitude Control Systems for CubeSat-Class Nanosatellite

Table 4

AFSMC controller parameters for air bearing testing.

NameValues

Sliding surface gain 0.00001, 100
Fuzzy membership function 1, 1
Adaptive gains 0.1, 0.36, 0.01, 2

AFSMC parameter 0.004

AFSMC parameter 0.0025

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