When lifting up a long slender beam from ground, the payload may slip or move suddenly in unintended and unpredictable ways. This occurs during crane operations when the movements of the overhead trolley and the hoist cable are not properly coordinated. Also, it is difficult to keep the centers of hook and payload mass aligned with the pivot point when the payload is lifted off the ground, resulting in undesired hook and payload swing. The payload’s unintended sliding or swing can potentially cause damage and reduce efficiency. This paper divides the lift-up process into two phases including a constrained phase and a free hanging phase, develops a combination of PID controller and speed envelope to prevent slip in the constrained phase, and presents an observer-based Linear Quadratic Regulator (LQR) control strategy to stabilize the double-pendulum oscillations in the free hanging phase. The robustness of the proposed observer-based LQR was analyzed. Lift-up experiments were carried out to verify the controller development.
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ASME 2018 Dynamic Systems and Control Conference
September 30–October 3, 2018
Atlanta, Georgia, USA
Conference Sponsors:
- Dynamic Systems and Control Division
ISBN:
978-0-7918-5191-3
PROCEEDINGS PAPER
Control of Slender-Beam Payloads During Lift-Up Operations
Shenghai Wang,
Shenghai Wang
Dalian Maritime University, Dalian, China
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William Singhose,
William Singhose
Georgia Tech, Atlanta, GA
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Yujia Yang
Yujia Yang
Georgia Tech, Atlanta, GA
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Shenghai Wang
Dalian Maritime University, Dalian, China
Aldo Ferri
Georgia Tech, Atlanta, GA
William Singhose
Georgia Tech, Atlanta, GA
Yujia Yang
Georgia Tech, Atlanta, GA
Paper No:
DSCC2018-8967, V003T40A003; 10 pages
Published Online:
November 12, 2018
Citation
Wang, S, Ferri, A, Singhose, W, & Yang, Y. "Control of Slender-Beam Payloads During Lift-Up Operations." Proceedings of the ASME 2018 Dynamic Systems and Control Conference. Volume 3: Modeling and Validation; Multi-Agent and Networked Systems; Path Planning and Motion Control; Tracking Control Systems; Unmanned Aerial Vehicles (UAVs) and Application; Unmanned Ground and Aerial Vehicles; Vibration in Mechanical Systems; Vibrations and Control of Systems; Vibrations: Modeling, Analysis, and Control. Atlanta, Georgia, USA. September 30–October 3, 2018. V003T40A003. ASME. https://doi.org/10.1115/DSCC2018-8967
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