Design method of aircraft control system

Abstract

The invention discloses a design method of an aircraft control system. The invention relates to the technical field of aircraft control. The system comprises an aircraft control end for controlling the flight condition of an aircraft, the input end of the aircraft control end is connected with a positioning digital model module used for data flight control. The input end of the positioning digitalmodel module is connected with a coordinate graph editing module used for establishing an equal-ratio coordinate graph in combination with a network map, an aircraft model editing module used for analyzing the flight mechanism of an aircraft and the structural size of the aircraft to establish a digital model, and a flight positioning selection module used for inputting flight target coordinates.And the output end of the positioning digital model module is connected with a flight path editing module for editing a flight path according to aircraft coordinates and input flight target coordinates. Flight path editing is carried out through coordinates, a simple coordinate positioning technology is adopted, visual flight state control is achieved, and the control mode is simple.

Description

technical field [0001] The invention relates to the technical field of aircraft control, in particular to an aircraft control system design method. Background technique [0002] Quadcopter is also called four-rotor aircraft and four-rotor helicopter, referred to as four-axis and four-rotor. This quadrotor is a multi-rotor aircraft. The four propellers of the quadcopter are simple mechanisms directly connected to the motors. The cross-shaped layout allows the aircraft to obtain the force of rotating the fuselage by changing the motor speed, thereby adjusting its own attitude. Specific technical details are described in "Basic Motion Principles". Because of its inherent complexity, there has never been a large commercial quadcopter in history. In recent years, thanks to the development of micro-electromechanical control technology, stable quadcopters have received widespread attention, and their application prospects are very promising. Nowadays, multi-copters with other ro...

AI Technical Summary

Problems solved by technology

[0004] To this end, an embodiment of the present invention provides a design method for an aircraft control system. By editing the flight path between the aircraft coordinates and the flight target coordinates, the positioning flight module of the aircraft performs flight control of the aircraft according to the flight path, and the positioning coordinates of the flight target can be Change the settings at any time, that is, change the flight path, realize the flight control of the aircraft, use simple coordinate positioning technology, realize intuitive flight state control, simple control mode, adapt to multi-rotor multi-axis aircraft, to solve the problem of aircraft control in the prior art Complicated calculations and problems caused by inconvenient aircraft control

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