An Improvement of PISS Integral Sliding Mode Control of Supersonic Missiles
2012 ◽
Vol 155-156
◽
pp. 1223-1226
Considering the pitch channel simplified model of supersonic missile system, a integral type of sliding surface is constructed with the error of overload and the integration of error and the angle speed signal. Base on the linear sliding mode, a simple PS adaptive integral sliding mode controller is designed In order to improve the performance of the proposed method, two improvements also proposed. Finally, a hybrid PISS adaptive control is formed which contains proportion control, integration control, the sign function and soft function.
2020 ◽
Vol 23
(3)
◽
pp. 249-259
Keyword(s):
2011 ◽
Vol E94-A
(4)
◽
pp. 1051-1058
◽
Keyword(s):
2020 ◽
Vol 0
(0)
◽
2021 ◽
Vol 1115
(1)
◽
pp. 012001
Keyword(s):
2022 ◽
Vol 134
◽
pp. 107481
2021 ◽
Vol 40
(5)
◽
pp. 1011-1031
2015 ◽
Vol 88
(10)
◽
pp. 2055-2065
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