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- W2369439351 abstract "In order to improve the flight qualities of carrier aircraft during launch vehicle separation,the state feedback system with state observer based on modern control theory was designed in order to get the expected close-loop apices,and linear control laws proportion to state variables were adopted.The feedback gain was calculated through the method called as Bass-Gura,and the time-domain method was applied to the simulation of long and short cycle modes.The results show that long and short cycle modes are both periodicity and convergence,and the flight quality satisfies grade one.Obviously the state feedback system is a very efficient and adapted method to improve flight qualities of aircraft." @default.
- W2369439351 created "2016-06-24" @default.
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- W2369439351 date "2012-01-01" @default.
- W2369439351 modified "2023-09-23" @default.
- W2369439351 title "Study on state feedback system to improve flight qualities of carrier aircraft during launch vehicle separation from aircraft" @default.
- W2369439351 hasPublicationYear "2012" @default.
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