Sliding Mode Observer and Controller Design for Nonlinear Supersonic Missile
2013 ◽
Vol 718-720
◽
pp. 1228-1233
Keyword(s):
The nonlinear equations of motion were constructed for a supersonic anti-warship missile. In order to estimate the unknown angle-of-attack, a sliding mode observer was designed. The convergence capability of the sliding mode observer was analyzed according to the Lyapunov stability theory. A sliding mode controller was designed to drive the missile normal overload output to track its command, based on the output-redefinition approach. In order to confirm the performance of the designed sliding mode observer and controller, a simulation example was carried out for nonlinear missile model. The simulation results show the fast convergence capability of the designed sliding mode observer and controller.
2013 ◽
Vol 2013
◽
pp. 1-7
◽
Keyword(s):
2018 ◽
Vol 32
(31)
◽
pp. 1850342
◽
2017 ◽
Vol 26
(4)
◽
pp. 697-715
◽
1994 ◽
Vol 116
(4)
◽
pp. 659-667
◽
2011 ◽
Vol 2011
◽
pp. 1-13
◽
2012 ◽
Vol 2012
◽
pp. 1-10
◽
2013 ◽
Vol 133
(5)
◽
pp. 1003-1009
Keyword(s):