Sliding Variable Structure Control for Attitude of Moving-Mass Hypersonic Vehicles
2013 ◽
Vol 325-326
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pp. 1225-1228
Keyword(s):
The moving-mass hypersonic attitude dynamic model is a strong nonlinear, multivariable, and strong coupling system. Based on the reasonable assumption, a simplified dynamic model is given. According to the time-scale separation theory, a sliding variable structure controller is designed and implemented for the tracking control of angular velocity and angle at the same time. Simulation results demonstrate the effectiveness of controller.
Keyword(s):
2011 ◽
Vol 383-390
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pp. 6931-6937
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2011 ◽
Vol 130-134
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pp. 1963-1967
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2013 ◽
Vol 303-306
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pp. 1228-1233
2020 ◽
2020 ◽
2020 ◽
2020 ◽