Multi-scale approximate explicit model predictive control method for three-degree-of-freedom helicopter

A technology of model predictive control and helicopter, applied in the direction of adaptive control, general control system, control/adjustment system, etc., can solve problems such as increasing complexity and increasing difficulty in dealing with problems, so as to overcome defects, facilitate online search and online Find handy effects

Inactive Publication Date: 2018-12-21
ZHEJIANG COLLEGE OF ZHEJIANG UNIV OF TECHOLOGY
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Problems solved by technology

However, when the number of inputs increases or the control time domain becomes longer, the

Method used

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  • Multi-scale approximate explicit model predictive control method for three-degree-of-freedom helicopter
  • Multi-scale approximate explicit model predictive control method for three-degree-of-freedom helicopter
  • Multi-scale approximate explicit model predictive control method for three-degree-of-freedom helicopter

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Embodiment Construction

[0068] The present invention will be further described below in conjunction with accompanying drawing:

[0069] The three-degree-of-freedom helicopter rapid model predictive control method of the present invention, such as figure 1 Shown is the application object three-degree-of-freedom helicopter model, figure 2 It is a three-degree-of-freedom helicopter system model diagram, and specifically includes the following steps:

[0070] Step 1) modeling the three-degree-of-freedom helicopter system to obtain the three-degree-of-freedom helicopter performance index function;

[0071] The space state equation of the three-degree-of-freedom helicopter system is:

[0072]

[0073] Select altitude angle ε, pitch angle p, rotation angle r, altitude angular velocity Pitch rate and the rotational angular velocity as a state vector, that is The voltage of the front and rear motors is taken as input, that is, u=[V f V b ] T , output y=[ε p r] T . By substituting the param...

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Abstract

The invention discloses a multi-scale approximate explicit model predictive control method for a three-degree-of-freedom helicopter. The multi-scale approximate explicit model predictive control method comprises the following steps that step (1), modeling is carried out on the three-degree-of-freedom helicopter to obtain a parameter optimization problem, namely an object to be approximated below;step (2), a piecewise linear insertion method is carried out to initially obtain an approximate control law; step (3), self-adaptive separation function approximation is carried out, and the form of the approximate control law is transformed; step (4), a barycenter function is introduced, and barycenter interpolation is utilized to obtain an approximate control law based on the barycenter function; and step (5), multi-scale approximate explicit model predictive control over a three-degree-of-freedom helicopter system is carried out. According to the multi-scale approximate explicit model predictive control method, the real-time performance of the three-degree-of-freedom helicopter control system is improved, the control complexity is reduced, the storage capacity requirement of a controller is reduced, the online calculation time is saved, and a good control effect is achieved.

Description

technical field [0001] The invention relates to an optimal control method of a flight controller. Background technique [0002] With the development of society, there are more and more types of means of transportation. Among them, aircraft has attracted widespread attention from the society due to its unique advantages. All countries in the world have increased investment in this field, and its development is also related to national security and strength. reflect. Among them, helicopters are special among various types of aircraft. They can quickly take off and land, and can adapt to difficult environments. Compared with traditional controllers, optimized controllers are particularly important. It is the key to system evaluation and analysis to run normally and reduce computing cost while improving system performance indicators. [0003] For dealing with multivariable constrained optimal control problems, model predictive control method is a very effective method. After y...

Claims

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Application Information

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IPC IPC(8): G05B13/04
CPCG05B13/042
Inventor 张聚吴崇坚赵恺伦陈伟杰周俊田峥
Owner ZHEJIANG COLLEGE OF ZHEJIANG UNIV OF TECHOLOGY
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