Modelling and Simulation of RKX200 Rocket Flight Dynamics

被引：0

作者：

Nurhafid, Alfi ^{[1
]}

Trilaksono, Bambang Riyanto ^{[1
]}

Sasongko, Rianto Adhy ^{[2
]}

Riyadl, Ahmad ^{[3
]}

Irwanto, Herma Yudhi ^{[3
]}

机构：

[1] Bandung Inst Technol, Dept Elect Engn, Bandung, Indonesia

[2] Bandung Inst Technol, Dept Aeronaut & Astronaut, Bandung, Indonesia

[3] Natl Inst Aeronaut Space, Dept Rocket Telemetry & Control Technol, Bandung, Indonesia

来源：

PROCEEDINGS OF 2013 3RD INTERNATIONAL CONFERENCE ON INSTRUMENTATION, COMMUNICATIONS, INFORMATION TECHNOLOGY, AND BIOMEDICAL ENGINEERING (ICICI-BME) | 2013年

关键词：

modelling; HILS; flight dynamics; simulation; flightgear;

D O I：

暂无

中图分类号：

R318 [生物医学工程];

学科分类号：

0831 ;

摘要：

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) 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 and simulated using Simulink (TM) while its motion visualization is constructed using FlightGear (TM). Further, the dynamics model and the visualization application then are integrated and tested in Hardware In The Loop Simulation (HILS) environment.

引用

页码：230 / 236

页数：7

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