Numerical Trajectory Optimization for Airborne Wind Energy Systems Describred by High-Fidelity Aircraft Models

• In order to study design tradeoffs in the development of an AWE system, it is useful to develop a code to optimize a trajectory for arbitrary objective function and constraints.We present a procedure for using direct collocation to optimize such a trajectory where a model is specified as a set of differential-algebraic equations. The six degree of freedom single-kite, pumping-mode AWE model developed in Chap. 10 is summarized, and two typical periodic optimal control problems are formulated and solved: maximum power and number of cycles per retraction. Finally a procedure for optimally transitioning between two fixed trajectories is presented.

Ämnesord

TEKNIK OCH TEKNOLOGIER  -- Elektroteknik och elektronik (hsv//swe)

ENGINEERING AND TECHNOLOGY  -- Electrical Engineering, Electronic Engineering, Information Engineering (hsv//eng)

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