Article Comments

Contributions from readers on our articles are very welcome. This form will let us retrieve the current data in the database and allows us to consider your comments.

Spacecraft attitude control using non-singular finite time convergence fast terminal sliding mode
Pyare Mohan Tiwari; S. Janardhanan; Masuq-un-Nabi
International Journal of Instrumentation Technology (IJIT), 2012 Vol.1 No.2, pp.124 - 142
11 - 19 =

Thank you for your feedback.

Return to top