Multi-granularity Modeling of Variable Structured Rocket based on Declarative Language

Wanmeng Zhou, Hua Wang, Fuyu Sun, Haiyang Li

2015

Abstract

The development of the rocket design process depends heavily on the effective and accurate modeling method. This paper elaborates the procedure to establish the variable structured rocket simulation package with the declarative modeling language Modelica. The package includes the rocket library with basic rocket components and rocket products with subsystems and segments. Some of the components like body and measurement take full advantages of the Modelica object-oriented characters, while others like control system and aerodynamics are assembled on the basis of traditional flight dynamics. The multi-granularity library for variable-structured rocket is verified with a case study. The results indicate that the library is successfully applied to the rocket modeling for flight control system design and is capable of rocket design in different phases.

References

  1. Alejandro, A., Perez, A., 2001. Modeling of a Gas Turbine with Modelica [D]. Sweden: Department of Automatic Control Lund Institute of Technology.
  2. Elmqvist, H., Brueck, D., Mattsson, S., et al, 1992. Dymola - Dynamic Modeling Laboratory User's Manual. Sweden: Dynasim AB.
  3. Ferretti, G., Schiavo, F., and Vigan, L., 2005. ObjectOriented Modeling and Simulation of Flexible Multibody Thin Beams in Modelica with the Finite Element Method. In Proceedings of the 4th international Modelica conference, pages 358-366, Modelica Association.
  4. Gertjan, L., 2008. The New DLR Flight Dynamics Library [C]. In Proceedings of the 6th International Modelica Conference, pages 193-202, Modelica Association.
  5. Moormann, D., Looye, G., 2002. The Modelica Flight Dynamics Library [C]. In Proceedings of the 2nd International Modelica Conference, pages 275-284, Modelica Association.
  6. Schiavo, F., Vigan, L., and Ferretti, G., 2006. Modular Modeling of Flexible Beams for Multibody Systems [J]. Multibody Systems Dynamics, 12(1):73- 88.
  7. Tiziano, P., Marco, L., 2005. Object-oriented Modeling of the Dynamics of a Satellite Equipped with Single Gimbal Control Moment Gyros [C]. In Proceedings of the 4th International Modelica Conference, pages 35- 44, Modelica Association.
  8. Zhang, S., Cheng W. K., Wang H., Tang G. J., 2010. Ballistic Missile System Simulation Based on Modelica [J]. Journal of Projectiles, Rockets, Missiles and Guidance, 30(5):21-30.
  9. Zhang, S., Cheng W. K., Wang H., Tang G.J., 2011. The Development of Ballistic Missile Model Library Based on Modelica [J]. Journal of Projectiles, Rockets, Missiles and Guidance, 31(3):2-5.
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Paper Citation


in Harvard Style

Zhou W., Wang H., Sun F. and Li H. (2015). Multi-granularity Modeling of Variable Structured Rocket based on Declarative Language . In Proceedings of the 5th International Conference on Simulation and Modeling Methodologies, Technologies and Applications - Volume 1: SIMULTECH, ISBN 978-989-758-120-5, pages 344-351. DOI: 10.5220/0005507703440351


in Bibtex Style

@conference{simultech15,
author={Wanmeng Zhou and Hua Wang and Fuyu Sun and Haiyang Li},
title={Multi-granularity Modeling of Variable Structured Rocket based on Declarative Language},
booktitle={Proceedings of the 5th International Conference on Simulation and Modeling Methodologies, Technologies and Applications - Volume 1: SIMULTECH,},
year={2015},
pages={344-351},
publisher={SciTePress},
organization={INSTICC},
doi={10.5220/0005507703440351},
isbn={978-989-758-120-5},
}


in EndNote Style

TY - CONF
JO - Proceedings of the 5th International Conference on Simulation and Modeling Methodologies, Technologies and Applications - Volume 1: SIMULTECH,
TI - Multi-granularity Modeling of Variable Structured Rocket based on Declarative Language
SN - 978-989-758-120-5
AU - Zhou W.
AU - Wang H.
AU - Sun F.
AU - Li H.
PY - 2015
SP - 344
EP - 351
DO - 10.5220/0005507703440351