Abstract
The control structure of the differential equations of a typical flight dynamical control problem is studied and methods for defining a relaxed problem with the aid of a least number of additional control parameters are presented. The usefulness of the relaxed problems for proving the existence of optimal solutions and calculating approximately optimal solutions is explained in detail.
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Bittner, L. (1998). On the Convexification of Optimal Control Problems of Flight Dynamics. In: Schmidt, W.H., Heier, K., Bittner, L., Bulirsch, R. (eds) Variational Calculus, Optimal Control and Applications. International Series of Numerical Mathematics, vol 124. Birkhäuser, Basel. https://doi.org/10.1007/978-3-0348-8802-8_1
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DOI: https://doi.org/10.1007/978-3-0348-8802-8_1
Publisher Name: Birkhäuser, Basel
Print ISBN: 978-3-0348-9780-8
Online ISBN: 978-3-0348-8802-8
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