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An anti-disturbance and parameter perturbation control method for asymptotically stable quadrotor UAV

An asymptotically stable and control method technology, applied in the field of control science and engineering, can solve problems such as complex algorithms, harsh constraints, and difficult engineering implementation, and achieve the effect of simple calculation, easy engineering implementation, and small algorithm scale

Inactive Publication Date: 2017-03-15
CIVIL AVIATION UNIV OF CHINA
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Problems solved by technology

[0004] A comprehensive analysis of the above-mentioned existing research results shows that there are the following unresolved problems: First, the existing anti-jamming control methods need specific information about external disturbances, such as the period and amplitude of disturbances, and this limited condition cannot be solved when the project is realized. It cannot be satisfied at all; second, the existing anti-interference or anti-parameter perturbation control methods generally require the disturbance or parameter perturbation to be constant or slowly time-varying. This constraint is too harsh and does not meet the actual situation. ; Third, the existing anti-interference or anti-parameter perturbation control methods have a large calculation scale and complex algorithms, which are difficult to implement in engineering

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  • An anti-disturbance and parameter perturbation control method for asymptotically stable quadrotor UAV
  • An anti-disturbance and parameter perturbation control method for asymptotically stable quadrotor UAV
  • An anti-disturbance and parameter perturbation control method for asymptotically stable quadrotor UAV

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[0053] The anti-interference and parameter perturbation anti-interference and parameter perturbation quadrotor UAV asymptotically stable control method provided by the present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0054] Such as figure 1As shown, the four-rotor UAV asymptotically stable control method of anti-interference and parameter perturbation provided by the present invention includes the following steps carried out in order:

[0055] (1) Establish a quadrotor UAV nonlinear mathematical model including external disturbance and internal parameter perturbation;

[0056] The structure of the four-rotor UAV body is as follows: figure 2 As shown, the corresponding nonlinear mathematical model is:

[0057]

[0058] where θ, φ and Represent real-time pitch, roll and yaw respectively, l represents the arm length from the center of gravity to each propeller axis, I x , I y with Represents ...

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Abstract

An anti-interference and parameter perturbation four-rotor UAV (unmanned aerial vehicle) asymptotically stable control method includes the steps: building a four-rotor UAV nonlinear mathematical model including external interference and internal parameter perturbation; setting a control target and constraint conditions needed by an asymptotically stable control algorithm; designing an external interference estimation algorithm; designing the asymptotically stable control algorithm. The control method has the advantages that interference compensation can be realized without specific information (such as interference cycle and amplitude) of the external interference, effective asymptotically stable control can be realized under the condition of coexistence of the external interference and internal parameter perturbation, both the external interference and internal parameter perturbation of a system can be rapidly time-varying (an abnormal value or slow time-varying type), the control method based on a nonlinear analysis model is attached with a strict theoretical proof (non-intelligent method or linear control methods such as fuzzy or neural network control), and the algorithm is small in scale, simple in operation and easy in engineering implementation.

Description

technical field [0001] The invention belongs to the field of control science and engineering, in particular to a four-rotor UAV asymptotically stable control method for anti-interference and parameter perturbation. Background technique [0002] In the past 20 years, quadrotor unmanned aerial vehicle (UAV) has been greatly developed due to its advantages of portability, maneuverability and wide application. However, there are many control problems in quadrotor UAV, such as: 1) weak anti-interference ability; 2) parameter perturbation inside the system model; 3) underactuation problem; 4) open-loop instability. [0003] In order to solve these problems, researchers have adopted a variety of modeling and control design methods to solve the above problems. For example, in 2010, R. Zhang et al. studied the problem of attitude control of quadrotor aircraft accompanied by a type of time-varying disturbance. They used an observer to estimate the external disturbance and designed a...

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05B13/04
Inventor 郭润夏白兰萍郭凯
Owner CIVIL AVIATION UNIV OF CHINA