Adaptive control method for quadrotor aircraft based on inverse proportional function enhanced power reaching law and fast terminal sliding surface

Abstract

A quadrotor adaptive control method based on an inverse proportional function-enhanced power reaching law and a fast terminal sliding surface, comprising the following steps: Step 1, determining from the body coordinate system based on the quadrotor to the inertial coordinates based on the earth The transfer matrix of the system; step 2, analyze the dynamic model of the quadrotor aircraft according to Newton Euler formula; step 3, calculate the tracking error, and design the controller according to the fast terminal sliding mode surface and its first derivative. The present invention combines inverse proportional function enhanced power approaching law sliding mode control and fast terminal sliding mode control, not only can increase the approaching speed when away from the sliding mode surface, but also reduce chattering, improve the rapidity of the system, and realize fast Stable control, while realizing the finite time control of the tracking error, solves the problem that the tracking error tends to 0 only when the time tends to infinity in the traditional sliding mode surface. At the same time, the boundary of interference is estimated through self-adaptation, which improves the stability of the system.

Description

technical field [0001] The invention relates to an adaptive control method of a quadrotor aircraft based on an inverse proportional function enhanced power reaching law and a fast terminal sliding mode surface. Background technique [0002] Due to the characteristics of simple structure, strong maneuverability and unique flight mode, quadrotor aircraft has attracted extensive attention from scholars and scientific research institutions at home and abroad, and has quickly become one of the hot spots in international research. Compared with fixed-wing aircraft, rotorcraft can lift vertically, has low environmental requirements, does not need a runway, reduces costs, and has huge commercial value. The development of aircraft has made many dangerous high-altitude operations easy and safe, deterring other countries in military terms, and greatly increasing work efficiency in civilian terms. Quadrotors are highly flexible, can achieve rapid transitions of motion and hovering at a...

AI Technical Summary

Problems solved by technology

[0004] In order to overcome the problem that the traditional sliding mode surface cannot realize finite time control and further accelerate the approaching speed of the reaching law and reduce chattering, the present invention adopts fast terminal sliding mode control and an enhanced power reaching law based on an inverse proportional function, The idea of ​​switching control avoids the singularity problem, accelerates the approach speed of the system to the sliding mode surface, reduces chattering, and realizes limited time control

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