DocumentCode
1794960
Title
Minimum jerk trajectory generation of a quadrotor based on the differential flatness
Author
Jing Yu ; Zhihao Cai ; Yingxun Wang
Author_Institution
Sci. & Technol. on Aircraft Control Lab., Beihang Univ., Beijing, China
fYear
2014
fDate
8-10 Aug. 2014
Firstpage
832
Lastpage
837
Abstract
In order to improve smoothness of task trajectories, this paper describe algorithms to generate smooth-optimal trajectories based on the differential flatness of quadrotor. B-spline is used to parameterize the selected flat outputs, and the dynamic constraints or kinematical constraints on quadrotor are transferred to the control point constraints of B-spline. The trajectory generation is then considered an optimal control problem by adopting the integral of squared jerk. And then the optimal solution is solved by transforming the optimal control problem into a nonlinear programming problem. At last the smoothness-optimal trajectories are generated. Simulation results show that, this method can smooth out movements and minimize the accumulative jerk which can decrease trajectory tracking errors effectively.
Keywords
helicopters; nonlinear programming; optimal control; splines (mathematics); trajectory control; B-spline; differential flatness; dynamic constraints; kinematical constraints; minimum jerk trajectory generation; nonlinear programming problem; optimal control problem; quadrotor; smooth-optimal trajectories; trajectory tracking errors; Aerospace electronics; Equations; Optimal control; Programming; Splines (mathematics); Trajectory; Vectors;
fLanguage
English
Publisher
ieee
Conference_Titel
Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
Conference_Location
Yantai
Print_ISBN
978-1-4799-4700-3
Type
conf
DOI
10.1109/CGNCC.2014.7007318
Filename
7007318
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