Cite
HARVARD Citation
Tiwari, P. et al. (2012). Spacecraft attitude control using non–singular finite time convergence fast terminal sliding mode. International journal of instrumentation technology. pp. 124-142. [Online].
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Tiwari, P. et al. (2012). Spacecraft attitude control using non–singular finite time convergence fast terminal sliding mode. International journal of instrumentation technology. pp. 124-142. [Online].