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- W1486007479 abstract "A new approach to the high performance missile autopilot design based on the nonlinear servomechanism theory is proposed. This approach coupled with the analytic gain scheduling leads to an effective means to account for the nonlinearity and uncertainty in the missile system." @default.
- W1486007479 created "2016-06-24" @default.
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- W1486007479 date "1993-06-01" @default.
- W1486007479 modified "2023-09-27" @default.
- W1486007479 title "Flight Control Design By Nonlinear Servomechanism Theory" @default.
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- W1486007479 doi "https://doi.org/10.23919/acc.1993.4792885" @default.
- W1486007479 hasPublicationYear "1993" @default.
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