DocumentCode
183800
Title
Soft-landing control by control invariance and receding horizon control
Author
Di Cairano, Stefano ; Ulusoy, Alphan ; Haghighat, S.
Author_Institution
Mitsubishi Electr. Res. Labs., Cambridge, MA, USA
fYear
2014
fDate
4-6 June 2014
Firstpage
784
Lastpage
789
Abstract
We propose a design for soft landing control based on control invariant sets and receding horizon control. Soft landing control, which is of interest in several applications in aerospace, transportation systems, and factory automation, aims at achieving precise positioning of a moving object to a target position, while ensuring that the maximum velocity decreases as the target is approached. The resulting soft contact avoids damages and wear. In this paper, we formulate appropriate constraints and recast soft landing control as the generation of an admissible trajectory of the constrained system. Then, we compute a control invariant set and design a receding horizon control law that forces the state to remain in such set. Thus, the trajectories generated by the controller achieve soft landing, regardless of the controller cost function and horizon, also when the dynamics are uncertain. We demonstrate our approach by a case study in transportation systems.
Keywords
aircraft landing guidance; control system synthesis; infinite horizon; trajectory control; velocity control; admissible trajectory; control invariant sets; maximum velocity; receding horizon control; soft-landing control; Dynamics; Robustness; Trajectory; Uncertainty; Vectors; Vehicle dynamics; Vehicles; Constrained control; Control applications; Predictive control for linear systems;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference (ACC), 2014
Conference_Location
Portland, OR
ISSN
0743-1619
Print_ISBN
978-1-4799-3272-6
Type
conf
DOI
10.1109/ACC.2014.6858787
Filename
6858787
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