Referenced Items are not available for this document.
Extended linearization is applied to a nonlinear model of a highly maneuverable missile. Hence, classical design rules, dictated by the classical aeronautical knowledge, are used to design a global nonlinear controller for the missile. Unlike many other papers on extended linearization, stability-even incremental stability-of the nonlinear closed loop is shown, so global properties are guaranteed, meanwhile only local properties were expected from the design methodology. Simulation results including some robustness tests are also presented
Published in:
American Control Conference, 1999. Proceedings of the 1999
(Volume:6
)
Date of Conference: 1999
- Page(s):
- 3743 - 3747 vol.6
- Meeting Date :
- 02 Jun 1999-04 Jun 1999
- ISSN :
- 0743-1619
- Print ISBN:
- 0-7803-4990-3
- INSPEC Accession Number:
- 6403015
- Conference Location :
- San Diego, CA
- Digital Object Identifier :
- 10.1109/ACC.1999.786196
- Product Type:
- Conference Publications
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