A copy of this work was available on the public web and has been preserved in the Wayback Machine. The capture dates from 2020; you can also visit the original URL.
The file type is
AIAA Guidance, Navigation, and Control Conference
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 thisdoi:10.2514/6.2015-1078 fatcat:tef6aoirjre7pag3iktxhowoxe