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- W2099541751 abstract "This paper describes the computer simulation and experimentation of a remotely controlled model aircraft under linear quadratic control. The aircraft is first modelled mathematically using Newton's laws and coordinate transformations which form a set of nonlinear differential equations. The mathematical model is linearized and used as the basis for the linear quadratic problem. The control system is simulated and then implemented on the remotely controlled aircraft. The aircraft performance greatly improved with the addition of model based linear quadratic control." @default.
- W2099541751 created "2016-06-24" @default.
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- W2099541751 date "2002-11-11" @default.
- W2099541751 modified "2023-09-27" @default.
- W2099541751 title "Linear quadratic optimal control for an experimental OHS aircraft" @default.
- W2099541751 cites W1522531528 @default.
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- W2099541751 doi "https://doi.org/10.1109/cca.2000.897543" @default.
- W2099541751 hasPublicationYear "2002" @default.
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