Quad-rotor unmanned helicopter explicit prediction control method based on loft optimization

A four-rotor UAV and pigeon group optimization technology, applied in the field of aircraft control, can solve the problems of difficult application of complex trajectories and high trajectory requirements, and achieve the effect of avoiding online optimization process, overcoming high trajectory requirements, and reducing control costs

Active Publication Date: 2016-06-08
BEIHANG UNIV
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AI Technical Summary

Problems solved by technology

[0061] This method uses the pigeon group algorithm to interpolate the trajectory and applies it to the explicit nonlinear model predictive control, which can overcome the problem that the nonlinear model predictive control has high requirements on the trajectory and the complex trajectory is difficult to apply, and avoids the problem of nonlinear model predictive control. The problem of multiple derivatives saves control costs

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  • Quad-rotor unmanned helicopter explicit prediction control method based on loft optimization
  • Quad-rotor unmanned helicopter explicit prediction control method based on loft optimization
  • Quad-rotor unmanned helicopter explicit prediction control method based on loft optimization

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Embodiment Construction

[0095] The effectiveness of the design method proposed by the present invention is verified below through a specific example of UAV target detection. The computer configuration of this experiment is i7-4710MQ processor, 2.50Ghz main frequency, 4G memory, and the software is MATLAB2014a version.

[0096] The specific implementation steps of this example are as follows:

[0097] Step 1: Establish the quadrotor UAV model and control quantity, give the required trajectory, and establish a display predictive control model. A simplified diagram of the quadrotor UAV is attached figure 1 , the body coordinate system xyz and the ground coordinate system XYZ are defined in the figure, and Euler angles are defined as attached figure 2 .

[0098] where the Euler angles are defined as follows:

[0099] Yaw angle Ψ: the angle between the projection of Ox on the plane OXY and the X axis

[0100] Pitch angle θ: the angle between the projection of Oz on the plane OXZ and the Z axis

[...

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Abstract

The invention discloses a quad-rotor unmanned helicopter explicit prediction control method based on heuristic bionic loft optimization. The method comprises the following steps that 1, a quad-rotor unmanned helicopter model is built according to aerodynamics and kinematics, and a relation between the controlled quantity and the state quantity is given; 2, a loft optimization algorithm is initialized, and the number D of sampling points required in a linearization track is given; 3, a cost function is designed; 4, map compass factors are utilized for optimization; 5, loft optimization landmark operators are utilized for optimization; 6, sample target points optimized by a loft are obtained to construct a linear interpolation function; 7, the interpolation function optimized by the loft is applied to the model obtained in the first step; 8, simulation or experiments are performed to obtain related results and verification. According to the method, the control complex difficulty can be lowered, the problem that explicit prediction control has the high requirement for the track and is hard to apply is solved, the online optimization process is avoided, a large amount of time is saved, and the control cost is lowered.

Description

【Technical field】 [0001] The invention is an explicit predictive control method for a quadrotor unmanned aerial vehicle based on heuristic bionic pigeon group optimization, belonging to the field of aircraft control. 【Background technique】 [0002] Unmanned Aerial Vehicle (UAV) plays an increasingly important role in today's military operations, and can effectively complete complex and dangerous reconnaissance and combat tasks. Although UAV has been widely used in military and civilian fields, many of its key technologies have yet to be further studied and applied. The quadrotor, as a cheaper and more reliable drone that can take off and land vertically, is being widely used in commercial and military applications. However, due to the multi-dimensionality of the quadrotor, it is controlled by four motors to take off and hover. Steering, so it requires a relatively high control rate. [0003] Model predictive control can realize precise control of the controlled object, but...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B13/04
CPCG05B13/042
Inventor 段海滨陈智隆邓亦敏
Owner BEIHANG UNIV
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