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- W4247100576 abstract "В работе рассматриваются две части: первая часть - разработка и моделирование системы управления мультироторным беспилотным летательным аппаратом, вторая часть – применение беспилотных летательных аппаратов в обеспечении технологической безопасности. Предложено использование математической модели мультироторного беспилотного летательного аппарата при построении системы управления. Беспилотный летательный аппарат рассматривается как объект управления, для которого необходимо решить задачу адаптации при построении маршрута. По причине маневренности и небольших габаритных размеров беспилотные летательные аппараты могут быть использованы для контроля крупногабаритных технологических аппаратов, трубопроводов в аварийных ситуациях или близких к ним.The use of the hexacopter mathematical model in the construction of a control system is proposed in this paper. An unmanned aerial vehicle is considered as a control object, for which it is necessary to solve the adaptation task when constructing a route.The aim of the research in this paper is to optimize the control of the UAV when constructing a flight route based on a mathematical model of a multi-rotor aircraft. This is due to the peculiarities of the movement of the multi-rotor UAV under various meteorological conditions.Multicopter (hexacopter) is described in sufficient detail in the literature. The position and orientation of the hexacopter in the earth’s coordinate system are determined by the three coordinates x, y, z and the three Euler angles. The positive directions of all turns correspond to counterclockwise rotation, along the axis of rotation to the origin.Based on the satellite navigation sensor data at the first stage, the initial and of course the state of the object are initiated, which will correspond to the required maneuver. The UAV route in the analytical form of the solution to the problem of finding the optimal speed control is based on the Pontryagin maximum principle. An alternative could be the extensive reversal method based on the Euler theorem on the final rotation of a rigid body having a fixed point." @default.
- W4247100576 created "2022-05-12" @default.
- W4247100576 creator A5068359107 @default.
- W4247100576 date "2019-10-26" @default.
- W4247100576 modified "2023-09-29" @default.
- W4247100576 title "Применение беспилотных летательных аппаратов в обеспечении технологической безопасности// Journal of Technical and Natural Sciences 5(14), 2019/ RELF Group & OEAPS Inc.(Open European Academy of Public Sciences); Chief Editor Vitaly Yakovlev- Berlin, Germany. 26.09.2019: OEAPS Inc., 2019. - PP. 54-90." @default.
- W4247100576 doi "https://doi.org/10.31219/osf.io/3yvd6" @default.
- W4247100576 hasPublicationYear "2019" @default.
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