Modelling and simulation of RKX200 rocket flight dynamics
In this paper, modelling and simulation of RKX200 rocket flight dynamics are presented. The dynamics model is constructed by first-principle method based on forces and moments acting the rocket rigid body. In the development of the model, the aerodynamics coefficients are determined by using missile...
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| creator | Nurhafid, Alfi Trilaksono, Bambang Riyanto Sasongko, Rianto Adhy Riyadl, Ahmad Irwanto, Herma Yudhi |
| description | In this paper, modelling and simulation of RKX200 rocket flight dynamics are presented. The dynamics model is constructed by first-principle method based on forces and moments acting 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) nonlinear 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 and simulated using Simulink™ while its motion visualization is constructed using FlightGear™. Further, the dynamics model and the visualization application then are integrated and tested in Hardware In The Loop Simulation (HILS) environment. |
| doi_str_mv | 10.1109/ICICI-BME.2013.6698498 |
| format | Conference Proceeding |
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The dynamics model is constructed by first-principle method based on forces and moments acting 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) nonlinear 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 and simulated using Simulink™ while its motion visualization is constructed using FlightGear™. Further, the dynamics model and the visualization application then are integrated and tested in Hardware In The Loop Simulation (HILS) environment.</abstract><pub>IEEE</pub><doi>10.1109/ICICI-BME.2013.6698498</doi><tpages>7</tpages></addata></record> |
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| language | eng |
| recordid | cdi_ieee_primary_6698498 |
| source | IEEE Electronic Library (IEL) Conference Proceedings |
| subjects | Aerodynamics Computational modeling Equations flight dynamics flightgear HILS Mathematical model modelling Numerical models Rockets simulation |
| title | Modelling and simulation of RKX200 rocket flight dynamics |
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