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- W2997262912 abstract "This paper describes a multi-objective flight control system design for ride quality improvement for flexible aircraft using multi-functional distributed flight control surfaces. A multi-objective optimal control design is developed to provide an acceleration suppression capability in conjunction with a gust load alleviation in order to provide ride quality improvement. A gust estimation is developed to estimate the gust load using a recursive least-squares algorithm. A ride quality assessment study is conducted using a flexible wing generic transport model. Six different flight control designs are implemented. The study shows that ride quality can be significantly improved with the acceleration suppression control." @default.
- W2997262912 created "2020-01-10" @default.
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- W2997262912 date "2020-01-05" @default.
- W2997262912 modified "2023-10-16" @default.
- W2997262912 title "Multi-Objective Flight Control for Ride Quality Improvement for Flexible Aircraft" @default.
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- W2997262912 doi "https://doi.org/10.2514/6.2020-1623" @default.
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