Attenuation of the effects produced by the bending modes of a flexible launch vehicle using second order filters
2020 ◽
Vol 2
(1)
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pp. 48-55
Keyword(s):
This article describes the application of an adaptive control algorithm for the atmospheric phase control of a launch vehicle. A dynamic model representing the pitch motion of the launch vehicle is introduced. As the bending modes can cause instability, the first threebending modes are modelled. A case study on design of the bending filters for a flexible launch vehicle using a model reference adaptive control is conducted to demonstrate its effectiveness.
2018 ◽
Vol 16
(11)
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pp. 5647-5670
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1994 ◽
Vol 141
(3)
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pp. 177-180
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1985 ◽
Vol 5
(5)
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pp. 303-307
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2005 ◽
Vol 219
(2)
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pp. 121-132
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