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- W2002952511 abstract "The Integral-LQ method was applied to the pitch loop autopilot design of a large flexible launch vehicle. The designs were evaluated based on their performance characteristics and robustness to model uncertainties and wind shear disturbances." @default.
- W2002952511 created "2016-06-24" @default.
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- W2002952511 date "1989-08-14" @default.
- W2002952511 modified "2023-09-26" @default.
- W2002952511 title "Application of integral-LQ to launch vehicle autopilot design" @default.
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- W2002952511 doi "https://doi.org/10.2514/6.1989-3459" @default.
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