Abstract:We consider the problem of generating an optimal aircraft reference trajectory in a horizontal plane, where the objective is to minimize exposure to a spatiotemporally varying scalar field. We consider a special case, where this field is timeinvariant, and we discuss optimal trajectory generation for an aircraft kinematic model based on first-and second-order necessary conditions of optimal control. Next, we consider the general case, with the additional assumption that the knowledge of this field is available… Show more
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