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Stability Certificates for a Model-Based Controller for Autonomous Power Kites

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Eva Ahbe PhD Researcher

ETH Zurich Automatic Control Laboratory

Physikstrasse 3, ETL K22.2 8092 Zurich Switzerland

ahbee@control.ee.ethz.ch www.control.ee.ethz.ch

Stability Certificates for a Model-Based Controller for Autonomous Power Kites

Eva Ahbe, Tony A. Wood, Roy S. Smith

ETH Zurich

One of the main challenges we are facing in AWE sys-tems research is the reliability of the controller for auto-matic flight operation of the kite within a given range of environmental conditions. Various control designs rang-ing from structurally simple model-free proportional-integral-derivative (PID) controllers to more complex model-based optimal control algorithms have been em-ployed for the automatic control of kites. Independent of the choice of controller, the challenge of assessing the re-liability remains. With rere-liability we refer to the guarantee of stably controlling the kite such that it does not diverge from a desired range of trajectories.

We propose an algorithm for controlling the crosswind flight in the energy-generating phase of a two-phase pumping cycle with guarantees of stability. The controller is based on a parameter varying linear quadratic regu-lator (LQR). For this model-based controller, we employ the kinematic model suggested by Wood et al. [1] to rep-resent the kite’s dynamics. In order to make our con-troller feasible in real time, LQR gains depending on the state of the kite, i.e., its position, heading and velocity, are computed offline. Similar to an approach proposed by Tedrake et al. [2], the control gains are stored in a so called LQR-tree library. Given an estimate of the kite state at any measurement instance, the corresponding stabilizing LQR gain can be recovered from the library. A crucial step for this library-based control scheme to guarantee stabil-ity is the assessment of the stabilizing region of the state space for each LQR gain. This information is obtained by performing a region of attraction (ROA) analysis for each gain. Our ROA analysis mainly follows the procedures proposed by Manchester [3]. The method is based on a

Lyapunov analysis where sums-of-squares programs are employed in order to obtain certificates of semi-algebraic set containment which guarantee stability for the consid-ered region. Using semi-definite relaxations, the set con-tainment problem is solved efficiently by a series of semi-definite programs. The obtained certificates allow us to choose a stabilizing controller gain at any instance such that the kite follows a predefined desired trajectory. The controller performance is sensitive to the accuracy of the state estimates. Measurements of the position and orientation of the kite from line angles or onboard sensors are often noisy and biased due to, e.g., line sag and time delays. In order to obtain more accurate mea-surements and improve the control performance, we are working on an active camera tracking system for state es-timation. The pan-tilt-zoom camera system is able to de-tect both the position of the kite in the wind window and its heading in real time. In this talk we will briefly highlight the benefits of this vision based estimation approach.

References:

[1] Wood, T. A., Hesse, H., Zgraggen, A. U. and Smith, R. S.: Model-Based Flight Path Planning and Tracking for Tethered Wings. 2015 IEEE Annual Conference on Decision and Control (CDC), IEEE, 6712-6717 (2015)

[2] Tedrake, R., Manchester, I. R., Tobenkin, M., & Roberts, J. W.: LQR-trees: Feedback Motion Planning via Sums-of-Squares Verification. The Intern. Journal of Robotics Research, 29(8), 1038-1052 (2010) [3] Manchester, I. R.: Transverse Dynamics and Regions of Stability for Nonlinear Hybrid Limit Cycles. IFAC Proceedings Volumes, 44(1), 6285-6290 (2011)

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