The need to track the motion trajectory, of a plane for example, the parameters of a power plant, etc., requires creating meters that operate under conditions of unpredictable changes in coordinates and their derivatives. This task is done by synthesizing tracking meters, which, depending on the situation, can change both the parameters and, possibly, the structure. This is implemented by meters, which can use different combinations of state models. In accordance with the chosen method, an algorithm for indicating the intensity of relative motion-aerodynamic object – measuring system- is obtained. The intensity is indicated by the acceleration magnitude of the aerodynamic object approach to the meter, calculated on the basis of information from meters of various physical nature.
Разработаны частные модели изменения дальности и скорости сближения квадрокоптера для случаев маневренного полета, неманевренного полета и зависания. Параметры предлагаемых частных моделей определены в результате проведенных натурных экспериментов. На основе этих моделей разработана обобщенная модель изменения дальности и скорости сближения квадрокоптера, применимая для описания изменения этих параметров движения в условиях его реального полета.
Particular models have been developed for changing the range and approach speed of a quadrocopter for the case of maneuverable flight, non-maneuverable flight and dependency. As a result of full-scale experiments, selective models are proposed. On the basis of the developed models, a generalized model for changing the range and approach speed of a quadrocopter is applicable to describe changes in motion parameters in the conditions of its real flight.
На основе экспериментальных данных, полученных в ходе имитационного моделирования наблюдения под разными ракурсами возду шного судна, движущегося по траектории типа «коробочка», разработана модель изменения его дальности и скорости сближения относительно наземной радиолокационной станции.
Abstract – On the basis of experimental data obtained in the course of simulation modeling of monitoring the movement of an aircraft moving along a “box” trajectory, a model was developed for changing its range and approach speed relative to a ground-based radar station.
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