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- W2324481965 abstract "This paper presents in brief, the techniques adopted for the development of a launch vehicle stage separation d ynamic simulator using object-oriented approach. The different co-ordinate frames, co-ordinate transformations, the force and moment modelling and the solution of equations of motion are discussed. These equations of motions are integrated b y Euler and fourth o rder Runge-Kutta schemes. The results are separation time versus relative gap d istance histories and the individual body attitudes. These results generated are used to predict the collision free separation of the rocket stages and payloads of the geo-synchronous, polar and low earth orbits. It is observed the predicted results were in close match with flight results." @default.
- W2324481965 created "2016-06-24" @default.
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- W2324481965 date "2003-09-29" @default.
- W2324481965 modified "2023-09-25" @default.
- W2324481965 title "Multibody Dynamic Simulator for Launch Vehicles Stage Separation Studies" @default.
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- W2324481965 doi "https://doi.org/10.2514/6.iac-03-a.6.08" @default.
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