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Design and verification method of aero-engine distributed control law considering time delay

An aero-engine and distributed control technology, which is applied in the direction of adaptive control, general control system, control/regulation system, etc., can solve problems such as high real-time requirements, meet multi-variable control requirements, reduce impact, and design methods are simple Effect

Active Publication Date: 2021-08-06
DALIAN UNIV OF TECH
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Problems solved by technology

[0007] At the same time, most of the existing aero-engine modeling and simulation work is carried out on the MATLAB / Simulink platform, but for the distributed control system, only using MATLAB for simulation has certain limitations, because the distributed Real-time requirements are high, and real-time network support is needed to simulate the topology, intelligent nodes and network communication conditions in the actual system

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  • Design and verification method of aero-engine distributed control law considering time delay
  • Design and verification method of aero-engine distributed control law considering time delay
  • Design and verification method of aero-engine distributed control law considering time delay

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Embodiment Construction

[0056] The present invention will be further described below in conjunction with accompanying drawing.

[0057] A control law design and verification method for an aeroengine distributed control system considering time delay, comprising the following steps:

[0058] S1. Discretize and augment the state-space model of the aeroengine distributed system with time delay, making it a standard discrete model without time delay in form;

[0059] S2. Design the ALQR controller for the augmented aeroengine distributed system model to realize the control of network delay in the distributed system;

[0060] S3. Build an aeroengine distributed control system simulation platform in the Truetime toolbox, and perform simulation verification on the designed ALQR controller;

[0061] Among them, the steps of discretization and augmentation modeling of the state space model of the aeroengine distributed system are as follows:

[0062] S1 first considers a certain type of turbofan engine, and ...

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Abstract

The invention belongs to the field of aero-engine control algorithm design, and proposes a method for designing and verifying a distributed control law of an aero-engine considering time delay. Modeling; designing the ALQR controller to control the network delay in the distributed system; building a simulation platform for the aero-engine distributed control system in the Truetime toolbox, and performing simulation verification on the designed ALQR controller. The method of the present invention can realize the control of the network time delay in the distributed system, and reduce the influence of the time delay on the performance of the engine; in addition, the control law design method for the distributed system with time delay has certain universality and can be extended to Other types of distributed time delay problems; at the same time, the parameters of the Truetime simulation platform provided by the invention are convenient to modify, and can perform simulation verification on other distributed control systems.

Description

technical field [0001] The invention proposes a control law design and verification method of an aeroengine distributed control system considering time delay, and belongs to the field of aeroengine control algorithm design. Background technique [0002] The background of the present invention is the design and verification of the control law for time delay of a certain type of turbofan engine distributed control system. [0003] The aircraft engine is the heart of the aircraft, and its performance is directly related to the flight safety of the aircraft. With the improvement of people's requirements for aero-engine control, the complexity of its control system design is also increasing, and the traditional centralized control architecture has been difficult to meet the complex control requirements. In order to further improve engine performance, reduce total engine weight, increase system versatility, and reduce system development and maintenance costs, the current aero-eng...

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05B13/04
CPCG05B13/042
Inventor 杜宪王欣悦孙希明马艳华
Owner DALIAN UNIV OF TECH
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