DocumentCode :
3527748
Title :
Trajectory generation and control of a quadrotor with a cable-suspended load - A differentially-flat hybrid system
Author :
Sreenath, Koushil ; Michael, Nathan ; Kumar, Vipin
fYear :
2013
fDate :
6-10 May 2013
Firstpage :
4888
Lastpage :
4895
Abstract :
A quadrotor with a cable-suspended load with eight degrees of freedom and four degrees underactuation is considered and the system is established to be a differentially-flat hybrid system. Using the flatness property, a trajectory generation method is presented that enables finding nominal trajectories with various constraints that not only result in minimal load swing if required, but can also cause a large swing in the load for dynamically agile motions. A control design is presented for the system specialized to the planar case, that enables tracking of either the quadrotor attitude, the load attitude or the position of the load. Stability proofs for the controller design and experimental validation of the proposed controller are presented.
Keywords :
aircraft control; attitude control; control system synthesis; helicopters; stability; trajectory control; cable-suspended load; control design; differentially-flat hybrid system; dynamically agile motions; flatness property; load attitude; nominal trajectories; quadrotor attitude; quadrotor control; stability proofs; trajectory generation method; Attitude control; Dynamics; Load modeling; Three-dimensional displays; Tracking; Trajectory; Vectors;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Robotics and Automation (ICRA), 2013 IEEE International Conference on
Conference_Location :
Karlsruhe
ISSN :
1050-4729
Print_ISBN :
978-1-4673-5641-1
Type :
conf
DOI :
10.1109/ICRA.2013.6631275
Filename :
6631275
Link To Document :
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