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.
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