Triggering-type predictive control-based aircraft control method

A technology of predictive control and control method, which is applied in the field of aircraft control to achieve the effects of improving the efficiency of online implementation, reducing the amount of online calculation, and improving stability

Inactive Publication Date: 2017-04-19
HUBEI UNIV OF TECH
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Problems solved by technology

At the same time, optimization is restricted by more factors. In addition to the constraints of physical conditions such as traditional actuators, various manufacturability, safety, economy (quality, energy consumption

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  • Triggering-type predictive control-based aircraft control method
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  • Triggering-type predictive control-based aircraft control method

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[0031] In order to better understand the present invention, the content of the present invention is further illustrated below in conjunction with the examples, but the content of the present invention is not limited to the following examples. Those skilled in the art can make various changes or modifications to the present invention, and these equivalent forms are also within the scope defined by the claims listed in this application.

[0032] The aircraft control method based on the trigger type predictive control adopted by the present invention firstly determines the optimal control sequence of the model predictive control algorithm at each sampling moment; then determines the conditional trigger equation of the conditional trigger mechanism through the output and state variables of the system; Finally, set the conditional threshold of the system according to the control requirements, and judge whether the system performs conditional triggering by comparing the magnitude rel...

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Abstract

The invention discloses a triggering-type predictive control-based aircraft control method. The method includes the following steps that: the optimal control sequence of a model predictive control algorithm at each sampling time point is determined; the condition triggering equation of a condition triggering mechanism is determined through the output and state variable of a system; and the condition threshold value of the system is set according to control requirements, whether the system should perform condition triggering is judged according to the comparison result of the value of the condition triggering equation and the threshold value at each sampling time point. According to the triggering-type predictive control-based aircraft control method of the invention, the model predictive control algorithm and the condition triggering mechanism are combined according to the problem of large on-line computation amount of a traditional model predictive control algorithm, and therefore, the computation amount of the model predictive control algorithm can be decreased, and the on-line implementation efficiency of the model predictive control algorithm can be improved.

Description

technical field [0001] The invention relates to an aircraft control method, in particular to an aircraft control method based on trigger-type predictive control. The method adds a conditional trigger mechanism on the basis of traditional model predictive control to solve the problem of online calculation of traditional model predictive control. Thereby improving its implementation efficiency in the aircraft control process, which belongs to the technical field of aircraft control. Background technique [0002] In recent years, with the development of unmanned aerial vehicle application technology, its control technology has gradually become the focus of the industry. Many scholars have also proposed many aircraft control methods: online optimal aircraft control system based on DHP algorithm, optimal control algorithm based on sliding mode control, backstepping quadrotor aircraft control system based on Lyapunov stability criterion. The online optimal aircraft control system...

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Application Information

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IPC IPC(8): G05D1/08
CPCG05D1/0825
Inventor 赵熙临刘斐明航吴胧胧何晶晶
Owner HUBEI UNIV OF TECH
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