Rabu, Juli 31, 2013

1st Paper

Abstract- In this paper, modelling and simulation of XXX rocket flight dynamics are presented. The dynamics model is constructed by first-principle method based on forces and moments acting at the rocket rigid body. In the development of the model, the aerodynamics coefficients are determined by using missile DATCOM software. A six Degree of Freedom (DoF) non-linear model, as well as linear decoupled longitudinal and lateral-directional models are constructed for representing the flight dynamics of the rocket. The resulting models are numerically modelled simulated using SimulinkTM while its motion visualization is constructed using FlightGearTM. Further, the dynamics model and the visualization application then are integrated and tested in Hardware In The Loop Simulation (HILS) environment.
Keyword: modeling, HILS, flight control, navigation, flightgear.--------------------------------------------------------------------------------------------------------------------------------------------

The citation above is my paper abstract. My paper discuss about modelling and simulation from one of rocket designed by National Institute of Aeronautics and Space. This paper not yet published by any institution, but I want to submit this paper into ICICI-BME the International Conference On Instrumentation, Communication, Information Technology and Biomedical Engineering. I hope this paper is acceptable.