Design and Simulation of High Altitude Air-Launched Automatic Underwater Vehicles

Article Preview

Abstract:

In this paper, an high altitude air-launched automatic underwater vehicles (AL-AUV) is designed based on the traditional torpedo-like AUV, REMUS. And an additional ex-range gliding wings unit is assembled on the top of AUV, which enable the AUV to be dropped at high altitude and gliding long distance to reach the signed investigating ocean field. The controllable surface on the wings also enhanced the controllability and flexibility of AUV gliding through the air and the ability against the influence of airflow interference. The AUV’s six DOF gliding model is established and a simulation system of AL-AUV is built with Matlab/Simulink. Analyzing the recorded simulation velocity and pitch characteristics of AL-AUV deployed at varying initial velocities and wing area, the optimized wing is selected.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

1386-1391

Citation:

Online since:

October 2011

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2012 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] Prestero, T., Development of a six-degree of freedom simulation model for the REMUS autonomous underwater vehicle, in Oceans 2001 MTS/IEEE - An Ocean Odyssey, 5-8 Nov. 2001: Honolulu, HI. pp.450-455.

DOI: 10.1109/oceans.2001.968766

Google Scholar

[2] Roe, S.M., Numerical and Experimental Analysis of Initial Water Impact of an Air-Dropped REMUS AUV. 2005, Master thesis of MIT & Woods Hole Oceanographic Institution.

DOI: 10.1575/1912/1519

Google Scholar

[3] Prestero, T., Verification of a six-degree of freedom simulation model for the REMUS autonomous underwater vehicle, in Department of Ocean Engineering and Mechanical Engineering. 2001, MIT and Woods Hole Oceanographic Institution: USA.

DOI: 10.1575/1912/3040

Google Scholar

[4] Doherr, K. and R. Synofzik. Investigations of rotating parachutes for submunitions. in AIAA 9th Aerodynamic Deceleration and Balloon Technology Conference. 1986. Albuquerque.

DOI: 10.2514/6.1986-2438

Google Scholar

[5] Dobrokhodov, V.N., O.A. Yakimenko, and C.J. Junge, Six-degree-of-freedom model of a controlled circular parachute. Journal of Aircraft, 2003. 40(3): pp.482-493.

DOI: 10.2514/2.3143

Google Scholar

[6] Robinson, A., On the use of quaternions in simulation of rigid-body motion. 1958, Wright Air Development Center.

Google Scholar

[7] Yakimenko, O.A. On the development of a scalable 8-DoF model for a generic parafoil-payload delivery system. in 18th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar, May 23, 2005 - May 26, 2005. 2005. Munich, Germany: American Institute of Aeronautics and Astronautics Inc.

DOI: 10.2514/6.2005-1665

Google Scholar

[8] Fossen, T., Guidance and control of ocean vehicles. Chichester New York, (1994).

Google Scholar