An Active Anti-jamming Tracking Control Method for Quadrotor UAV Circular Trajectory

A four-rotor UAV and tracking control technology, applied in the field of flight control, can solve problems such as harsh interference assumptions and restrict engineering applications, and achieve the effects of reducing adjustment difficulty, improving tracking accuracy and broad application prospects.

Active Publication Date: 2020-09-15
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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Problems solved by technology

However, the anti-disturbance performance of the existing robust control strategy is obtained at the expense of the nominal performance of the system, and the active anti-disturbance control strategy based on the extended state observer can obtain a good control effect, but its effect on the disturbance Assumptions are too harsh, which greatly limits its engineering application

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  • An Active Anti-jamming Tracking Control Method for Quadrotor UAV Circular Trajectory
  • An Active Anti-jamming Tracking Control Method for Quadrotor UAV Circular Trajectory
  • An Active Anti-jamming Tracking Control Method for Quadrotor UAV Circular Trajectory

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Embodiment Construction

[0059] The technical solutions of the present invention will be described in detail below in conjunction with the accompanying drawings.

[0060] The present invention designs an active anti-jamming tracking control method for a circular track of a four-rotor UAV, such as figure 1 As shown, the basic steps are as follows:

[0061] Step 1: Establish the position system model of the quadrotor UAV, and transform the trajectory tracking problem of the quadrotor UAV into the stabilization problem of the tracking error of the position loop;

[0062] Step 2: Introduce virtual control variables and establish a high-order sliding mode disturbance observer for the position subsystem of the quadrotor UAV;

[0063] Step 3: Establish a composite nonlinear dynamic inverse controller for the quadrotor UAV to ensure that the position system of the disturbed quadrotor UAV dynamically and progressively track its reference trajectory;

[0064] Step 4: Transform the virtual control quantity int...

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Abstract

The invention discloses an active anti-disturbance tracking control method for a circular trajectory of a quad-rotor unmanned aerial vehicle. The active anti-disturbance tracking control method comprises the steps of: establishing a quad-rotor unmanned aerial vehicle position system model, and converting a trajectory tracking problem of the quad-rotor unmanned aerial vehicle into a stabilization problem of a position loop tracking error; introducing a virtual control quantity, and establishing a quad-rotor unmanned aerial vehicle position subsystem high-order sliding mode disturbance observer;establishing a quad-rotor unmanned aerial vehicle composite nonlinear dynamic inverse controller, and ensuring that a disturbed quad-rotor unmanned aerial vehicle position system dynamically and progressively tracks a reference trajectory thereof; and converting the virtual control quantity into a real control quantity of the quad-rotor unmanned aerial vehicle through algebraic conversion. According to the active anti-disturbance tracking control method, the lumped disturbance of the system can be observed within limited time and dynamically compensated, so that the quad-rotor unmanned aerialvehicle has better anti-disturbance performance and robustness.

Description

technical field [0001] The invention belongs to the technical field of flight control, and in particular relates to a control method for a quadrotor unmanned aerial vehicle. Background technique [0002] Quadrotor UAV is a kind of UAV that can take off and land vertically and hover in the air. Due to its simple structure, convenient control, strong versatility of flight environment, and low maintenance cost, it has been widely used in aerial reconnaissance, high-altitude Photography, environmental disaster monitoring, disaster rescue and other fields have important research significance and application prospects. In the field of control theory research, quadrotor UAV system control is a typical benchmark problem with multiple input-multiple output, obvious nonlinear characteristics, and serious state coupling. In addition, the flight process of quadrotor drones will also be affected by multi-source interference such as internal aerodynamic parameter perturbation, friction a...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05D1/12
CPCG05D1/12
Inventor 赵振华曹东李春涛张朋路红飞邵海龙
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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