DocumentCode
3139246
Title
Reducing swing of model helicopter sling load using input shaping
Author
Potter, James ; Singhose, William ; Costello, Mark
Author_Institution
George W. Woodruff Sch. of Mech. Eng., Georgia Inst. of Technol., Atlanta, GA, USA
fYear
2011
fDate
19-21 Dec. 2011
Firstpage
348
Lastpage
353
Abstract
Helicopter sling-load operations are extremely useful, but they can also be dangerous. Excessive swinging of the load can degrade control, cause the payload to collide with obstacles, or allow the suspension cable to get tangled with objects. Suppressing load swing could increase safety and productivity. Input shaping is a control technique that has been used to suppress vibration of flexible machines, such as robots, satellites, and cranes. To investigate the use of input shaping on helicopters, a dynamic model is formed to characterize the translational response of a model helicopter and sling load to lateral control inputs. This translational model is used to simulate point-to-point movements with and without input shaping for a range of move distances. The input-shaped movements show greatly-reduced residual swing, with only a minor increase in move time. Data from an experimental trial using a model helicopter is presented.
Keywords
helicopters; vibration control; dynamic model; excessive swinging; helicopter sling-load operations; input shaping; model helicopter sling load; translational model; translational response; Cranes; Damping; Helicopters; Load modeling; Mathematical model; Robustness; Vibrations;
fLanguage
English
Publisher
ieee
Conference_Titel
Control and Automation (ICCA), 2011 9th IEEE International Conference on
Conference_Location
Santiago
ISSN
1948-3449
Print_ISBN
978-1-4577-1475-7
Type
conf
DOI
10.1109/ICCA.2011.6138048
Filename
6138048
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