Study on UAV Flight State Simulation

Abstract

Flight state is an important research content of UAV technology, it involves many factors, and simulation is very difficult. Based on the knowledge of relevant mathematical knowledge and flight control theory, a UAV flight control simulation method is proposed. The method combining sampling step and Gaussian white noise sampling values, UAV flight state parameters at each sampling point and output of the flight state parameters are obtained by iterative methods. This method is simple and practical, and it meets the needs of the UAV flight state simulation in the large-scale system simulation.