Strong anti-interference compound control method for overcoming influence of periodic moving part

A technology of composite control and moving parts, which is applied in the direction of motor vehicles, space navigation equipment, space navigation aircraft, etc., can solve the problems that the stability of the system is not easy to guarantee, and achieve the effect of good anti-interference effect

Active Publication Date: 2021-09-17
BEIJING INST OF CONTROL ENG
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  • Claims
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Problems solved by technology

[0003] For unknown periodic disturbances, the existing control methods are mainly divided into three categories: 1) When the disturbance cannot be measured but the period is known, the repetitive control based on the internal model principle is generally used, which is a kind of feedback control, but there are large When the dynamics are not modeled, the stability of the system is not easy to guarantee; 2) When the disturbance can be directly measured or known in advance (these conditions are usu

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  • Strong anti-interference compound control method for overcoming influence of periodic moving part
  • Strong anti-interference compound control method for overcoming influence of periodic moving part
  • Strong anti-interference compound control method for overcoming influence of periodic moving part

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[0110] Taking a satellite with a flywheel as an executive component as an example, the specific implementation of the present invention will be introduced. Take satellite pitch axis control as an example to illustrate. Assuming that the inertia of the satellite pitch axis is 5000kg.m2, the maximum combined moment of the flywheel group on the pitch axis is 0.2Nm. The moving part on the satellite is SADA, which is driven by a stepper motor through a reduction gear, and its motion period Δt d =4.32s, the maximum moment T acting on the star d,max About 0.1Nm, the dynamic process of single-step motion is about 1s. The controller sampling period h=0.1s. The following technical points and calculation formulas are realized by the onboard software and calculated in real time. figure 2 This is a schematic structural diagram of a strong disturbance immunity composite control system provided by an embodiment of the present invention. In this system,

[0111] (1) Using the fast Four...

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Abstract

The invention relates to a strong anti-interference compound control method for overcoming influences of a periodic moving part, and belongs to the field of spacecraft attitude control. The method comprises the following steps: estimating periodic interference by comprehensively utilizing fast Fourier transform (FFT) and an extended state observer (ESO), designing an equivalent feed-forward compensation law according to an angular momentum conservation principle on this basis, adjusting a disturbance torque feed-forward compensation moment value by utilizing a fuzzy logic system, and dynamically adjusting the gain of a PID controller according to whether the disturbance torque is in a feed-forward compensation period or not. Compared with an existing method, the method has the advantages that system identification is not needed, excessive model prior knowledge is not needed, and a good anti-interference effect is achieved through a simple control law; and the method is used for satellite attitude control with periodic interference, and attitude control precision and attitude stability of the system can be effectively improved. The whole method is high in systematicness, clear in process and easy to implement.

Description

technical field [0001] The invention belongs to the field of spacecraft attitude control, and relates to a strong anti-disturbance composite control method for overcoming the influence of periodic moving parts. Background technique [0002] Large and long-lived satellites usually carry many different types of payloads, and the satellite dynamic characteristics are complex and control requirements are high. For imaging payloads, the attitude stability of the satellite platform is an important technical indicator. Under the influence of various interference factors such as flexible vibration, liquid sloshing, and component motion, it is difficult to improve the attitude stability of the star. Among the many interference sources on the satellite, the low-frequency motion interference of periodic moving parts is common and has a significant impact. Common periodic moving parts on the star include scanning cameras, scanning antennas, solar windsurfing drive mechanism (SADA) and...

Claims

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Application Information

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IPC IPC(8): B64G1/24
CPCB64G1/244B64G1/245
Inventor 王佐伟何刚李建平李乐尧甘永石恒姚蘅沈扬帆王青贾涛于淑晶高秀娟
Owner BEIJING INST OF CONTROL ENG
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