{'fraction_non_alphanumeric': 0.009478672985781991, 'fraction_numerical': 0.0, 'mean_word_length': 6.041666666666667, 'pattern_counts': {'":': 0, '<': 0, '<?xml version=': 0, '>': 0, 'https://': 0, 'lorem ipsum': 0, 'www.': 0, 'xml': 0}, 'pii_count': 0, 'substrings_counts': 0, 'word_list_counts': {'cursed_substrings.json': 0, 'profanity_word_list.json': 0, 'sexual_word_list.json': 0, 'zh_pornsignals.json': 0}}
Synthesis of Optimal System with a Variable Structure for Control of Quadrotor UAV

The control of transient processes of a quadrotor unmanned aerial vehicle, described by ordinary nonlinear differential equations, requires the development of optimal systems with variable structure. The solution to this problem is suggested using a procedure for constructing optimal trajectories, determining switching moments and synthesizing control functions for multidimensional systems. The creation of algorithms and circuit solutions for the synthesis of optimal variable-structure systems for multidimensional nonlinear moving objects has practical significance as a basis for the formation of automated procedures for the synthesis of robust-optimal control systems and the development of software tools for various types of unmanned aerial vehicle.