2015
DOI: 10.1016/j.ifacol.2015.08.068
|View full text |Cite
|
Sign up to set email alerts
|

Adaptive SDRE Based Boost-Phase Missile Autopilot Design Using Single and Modular Neural Networks

Abstract: Adaptive autopilot is designed using State-Dependent Riccati Equation (SDRE) and Neural Networks (NN), which guarantees the control performance during the boost-phase of missile. Rapid changes of parameters and aerodynamic uncertainties degrade the control performance of missile during the boost-phase. To deal with the nonlinearity of the missile system due to the rapid changes of parameters, SDRE technique is adopted to design baseline controller, and to compensate the effects of aerodynamic uncertainties, mo… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...

Citation Types

0
0
0

Year Published

2016
2016
2018
2018

Publication Types

Select...
3

Relationship

0
3

Authors

Journals

citations
Cited by 3 publications
references
References 4 publications
0
0
0
Order By: Relevance