Control method for improving robustness of steering engine dynamic stiffness test system

A technology of system robustness and control method, which is applied in the control field of improving the robustness of the rudder maneuvering stiffness test system, can solve the problems of poor robustness, uncommanded position disturbance, and inability to achieve satisfaction, and achieves improved force tracking. Effects of improved accuracy, robustness, and wide perturbation range

Pending Publication Date: 2020-04-14
JIANGXI HONGDU AVIATION IND GRP
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Problems solved by technology

[0002] The rudder motor stiffness test system is a feedback control system. In the process of applying force loading, the loaded object is ideally at a fixed position. However, in the actual test process, the loaded object has certain abnormalities in the low-frequency loading stage Command position disturbance, the root cause of this phenomenon is that there is strong interference between the internal and external environment on the main control valve spool / motor controller
This results in the inability to accurately track the loading force, and brings certain difficulties to the analysis of the dynamic stiffness data at the low frequency stage
At the same time, when the rudder motor stiffness test system is used for different types of loaded objects, the degree of position disturbance is also quite different. Adjusting the control parameters of the rudder motor stiffness test system cannot achieve satisfactory results, and the robustness is poor.

Method used

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  • Control method for improving robustness of steering engine dynamic stiffness test system

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Embodiment Construction

[0014] The following will combine figure 1 , clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only a specific embodiment of the present invention, not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0015] Such as figure 1 As shown, the control system mainly includes a negative feedback loop and a positive feedback superposition loop. The specific control principle is:

[0016] Step1: The command F1 and the force sensor feedback value F2 form a negative feedback, and the difference e1 enters the PI controller for proportional and differential calculations to obtain the value K1;

[0017] Step2: Lead out the main control valve spool position command / motor movement command from the main control valve / motor...

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Abstract

The invention provides a control method for improving robustness of a steering engine dynamic stiffness test system. The principle is as follows: a feedback system is added in the steering engine dynamic stiffness test system, an instruction of a main control valve core / motor controller for controlling the position change of a loaded object actuating mechanism is extracted, a feedback signal is formed after certain processing, and the feedback signal is integrated with a loading instruction signal to control the loaded object actuating mechanism. The method is suitable for force tracking precision applied to a low-frequency (0.1 Hz to 8 Hz) loading stage, and a more satisfactory test effect can be obtained by adjusting control parameters of the steering engine dynamic stiffness test systemfor different loaded objects. According to the control method, the trouble caused by non-instructive position disturbance is solved, the control method is suitable for different loading objects, andthe robustness of the system is improved.

Description

technical field [0001] The invention belongs to the field of automatic control, in particular to a control method for improving the robustness of a rudder motor stiffness test system. Background technique [0002] The rudder motor stiffness test system is a feedback control system. In the process of applying force loading, the loaded object is ideally at a fixed position. However, in the actual test process, the loaded object has certain abnormalities in the low-frequency loading stage Command position disturbance, the root cause of this phenomenon is that there is strong interference between the internal and external environment on the main control valve spool / motor controller. As a result, the loading force cannot be accurately tracked, which brings certain difficulties to the analysis of the dynamic stiffness data at the low frequency stage. At the same time, when the rudder motor stiffness test system is used for different types of loaded objects, the degree of position...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F5/60G01M99/00
CPCB64F5/60G01M99/007
Inventor 谭磊胡海英梁琼花裴登洪殷晓华朱辉杰王晓坤武琳曾嵘翁雪花
Owner JIANGXI HONGDU AVIATION IND GRP
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