Quadrotor Rapid Modeling and Design Method Based on Editable Configuration Parameters Interface

Abstract

The invention discloses a quadrotor rapid modeling design method based on a programmable configuration parameter interface. The quadrotor rapid modeling design method is characterized by comprising the following steps: 1, establishing a kinetic model, including a variable module, an XML configuration file analysis module and a state resolving module; 2, defining a parameter XML file; 3, according to movement decomposition of a quadrotor aircraft, dividing movement of the quadrotor aircraft into transverse later movement and longitudinal movement, and respectively editing state resolving equations of the transverse later movement and the longitudinal movement; 4, designing a resolving program of the XML configuration file; 5, under the fixed condition that quadrotor aircrafts are symmetrically uniformly distributed, complexing a same kinetic model for different quadrotor aircrafts, modifying configuration parameters of the quadrotor aircrafts in the XML files, and re-resolving the configuration parameters into the kinetic model. By adopting the quadrotor rapid modeling design method, the use time can be greatly shortened, and the user development period can be shortened.

Description

technical field [0001] The invention belongs to the field of computer aircraft performance simulation, and in particular relates to a rapid modeling and design method for a quadrotor unmanned aerial vehicle based on an editable configuration parameter interface. Background technique [0002] Quadrotor UAV modeling is a complex and time-consuming process. When users conduct research on quadrotor UAVs, the first task they face is to mathematically model the quadrotor UAV. Mathematical models It is the basis for carrying out research work, because the mechanism modeling process of the quadrotor UAV is fixed, that is, the mathematical equation form that its mathematical model (the application of the present invention refers to the dynamic model) contains is fixed. Only the relevant parameters that reflect the attributes of the quadrotor UAV in the equation are changed, such as the body mass of the quadrotor UAV, the rotor lift coefficient, the rotor mass, the drag coefficient, t...

AI Technical Summary

Problems solved by technology

[0004] The present invention provides a rapid modeling and design method for quadrotor drones based on an editable configuration parameter interface, so as to solve the problems of repetitive labor, low work efficiency, and long quadrotor drones existing in the prior art. Problems such as the model development cycle of the UAV have greatly shortened the user's time in the UAV modeling process, thereby greatly reducing the user's quadrotor UAV model development cycle

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