DocumentCode :
1401994
Title :
Approximate Analytical Turning Conditions for Underwater Gliders: Implications for Motion Control and Path Planning
Author :
Mahmoudian, Nina ; Geisbert, Jesse ; Woolsey, Craig
Author_Institution :
Dept. of Aerosp. & Ocean Eng., Virginia Polytech. & State Univ., Blacksburg, VA, USA
Volume :
35
Issue :
1
fYear :
2010
Firstpage :
131
Lastpage :
143
Abstract :
This paper describes analysis of steady motions for underwater gliders, a type of highly efficient underwater vehicle which uses gravity for propulsion. Underwater gliders are winged underwater vehicles which locomote by modulating their buoyancy and their attitude. Several underwater gliders have been developed and have proven their worth as efficient long-distance, long-duration ocean sampling platforms. Underwater gliders are so efficient because they spend much of their flight time in stable, steady motion. Wings-level gliding flight for underwater gliders has been well studied, but analysis of steady turning flight is more subtle. This paper presents an approximate analytical expression for steady turning motion for a realistic underwater glider model. The problem is formulated in terms of regular perturbation theory, with the vehicle turn rate as the perturbation parameter. The resulting solution exhibits a special structure that suggests an efficient approach to motion control as well as a planning strategy for energy efficient paths.
Keywords :
approximation theory; mobile robots; motion control; path planning; perturbation techniques; underwater vehicles; approximate analytical turning condition; motion control; ocean sampling platform; path planning; regular perturbation theory; steady motions analysis; steady turning flight; steady turning motion; underwater glider; wings level gliding flight; Motion control; path planning; steady motion; underwater glider;
fLanguage :
English
Journal_Title :
Oceanic Engineering, IEEE Journal of
Publisher :
ieee
ISSN :
0364-9059
Type :
jour
DOI :
10.1109/JOE.2009.2039655
Filename :
5404981
Link To Document :
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