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- W2382816810 abstract "Firstly,the basic principle of aerocraft auto flatten-out system was simply depictioned,level fly trajec tory and exponential rule were analyzed.Secondly,the auto pullout coupler and auto changed level landing sys tem were designed.Lastly,under the MATLAB platform,the structure diagram of aero auto changed level fly system was established.A great deal of simulation researches was done.Simulation results indicated that the structure of designed auto flatten-out system and it’s coupler was reasonable,and the control system was stabili ty,and could meet demand for scheduled landing parameters" @default.
- W2382816810 created "2016-06-24" @default.
- W2382816810 creator A5060484787 @default.
- W2382816810 date "2013-01-01" @default.
- W2382816810 modified "2023-09-25" @default.
- W2382816810 title "Design and Simulation on Aerocraft Auto Flatten-Out and Landing System" @default.
- W2382816810 hasPublicationYear "2013" @default.
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