Investigation of robust adaptive control laws for flight control system implementation

A direct model-following adaptive concept is used to develop control laws for helicopter flight control systems (FCSs). The robust performance of the adaptive control scheme subject to parameter variations and system nonlinearity effects is demonstrated. The scheme provides an attractive solution to...

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Bibliographic Details
Published inIEEE Conference on Control Applications, 1992 pp. 608 - 610 vol.2
Main Authors Lam, Q.M., Hill, J.P.
Format Conference Proceeding
LanguageEnglish
Published IEEE 1992
Subjects
Adaptive control
Aerospace control
Aircraft
Error correction
Helicopters
Identity-based encryption
Integral equations
Noise figure
Programmable control
Robust control
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ISBN9780780300477
0780300475
DOI10.1109/CCA.1992.269780

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Summary:A direct model-following adaptive concept is used to develop control laws for helicopter flight control systems (FCSs). The robust performance of the adaptive control scheme subject to parameter variations and system nonlinearity effects is demonstrated. The scheme provides an attractive solution to FCS implementation for a modern attack helicopter with a minimal amount of software impact.< >
ISBN:9780780300477
0780300475
DOI:10.1109/CCA.1992.269780