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- W2978001716 abstract "For the study of dynamic characteristics of certain Unmanned Aerial Vehicle(UAV) with boosting rocket in the launching take-off phase,a dynamic model of the UAV launching system is established and simulated.According to the real structure of the UAV and the actual emission situation,a three-dimensional solid model of the UAV launching system is established,and then it is imported into the ADAMS,also the multi-body dynamics method is adopted to carry out dynamic simulation analysis for UAV Simulation Model.From the analysis of the simulation results,it was obtained that there is a suitable rocket installation angle and the emission angle of the UAV that can take off smoothly,which can provide references for UAV launching technology." @default.
- W2978001716 created "2019-10-10" @default.
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- W2978001716 date "2013-01-01" @default.
- W2978001716 modified "2023-09-24" @default.
- W2978001716 title "The Dynamic Simulation on Launching Phase for Unmanned Aerial Vehicle with Rocket Booster" @default.
- W2978001716 hasPublicationYear "2013" @default.
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