Abstract
The overload control of missile system is researched under the condition that the control direction is unknown. A nussbaum gain strategy is adopted to solve the unknown control direction problem for the linear model of missile motion of pitch channel . The backstepping technology and integral action are used to cope the system uncertainty. A novel type of control law, which is only consisted of overload signal and angle velocity of missile, is constructed and the stability of whole system is guaranteed by a whole Lyapunov function. The defect of the proposed method is that the dyanmic of control fin is not considered.
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© 2011 Springer-Verlag Berlin Heidelberg
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Shi, J., Zhao, G., Lei, J., Liang, G. (2011). Research on Backstepping Nussbaum Gain Control of Missile Overload System. In: Lin, S., Huang, X. (eds) Advances in Computer Science, Environment, Ecoinformatics, and Education. CSEE 2011. Communications in Computer and Information Science, vol 214. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-23321-0_96
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DOI: https://doi.org/10.1007/978-3-642-23321-0_96
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-23320-3
Online ISBN: 978-3-642-23321-0
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