Adaptive vibrating control method based on sailboard flexible deformation measurement

A technology of adaptive control and flexible deformation, applied in the direction of adaptive control, general control system, control/adjustment system, etc., can solve the problems of complex mode identification algorithm, sacrifice of dynamic characteristics, occupying satellite computing resources, etc., to achieve High-precision attitude control, avoiding information loss, and good reflection effects

CN102880049BActive Publication Date: 2015-04-22BEIJING INST OF CONTROL ENG
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Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Publication Date
2015-04-22

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Abstract

The invention provides a adaptive vibrating control method based on sailboard flexible deformation measurement. The adaptive vibrating control method comprises the following steps: (1) acquiring the deformation displacement of the root, the middle part and the end of a sailboard at the current time; (2) acquiring the attitude angular velocity of a spacecraft at the current time and the expected attitude angular velocity; (3) calculating the deviation of the attitude angular velocity based on the attitude information at the current time; (4) determining the adaptive controlling quantity of the spacecraft according to the deviation of the attitude angular velocity calculated in the step (3) and the quantity obtained in the step (1); and (5) controlling the spacecraft based on the proportional controlling quantity, the differential controlling quantity and the adaptive control quantity determined in the step (4); and turning to the step (1) to circularly operate all the steps at the next time, so as to achieve the adaptive vibrating control of the spacecraft based on the sailboard flexible deformation measurement.
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Description

technical field

[0001] The invention belongs to the field of spacecraft attitude control, and relates to an adaptive vibration control method based on sailboard flexible deformation measurement. Background technique

[0002] Modern spacecraft often have flexible appendages with lightweight structures such as large solar panels. The vibration of the flexible appendage during maneuvering at a large angle of attitude brings great difficulty to the stability of the attitude in a short period of time. Therefore, the vibration control of the sailboard during the rapid maneuvering process is a problem that must be solved. In addition, since it is difficult to accurately know the sailboard mode on the ground, the control parameters cannot be set completely in advance. For the situation where the flexible mode of the sailboard is uncertain, the usual method is to obtain the estimated value of the sailboard mode through ground or on-orbit identification, and then design an adaptive ...

Examples

Embodiment Construction

[0022] For complex spacecraft with large flexible appendages, the suppression of sailboard flexural vibration is an important means to improve the control accuracy of the spacecraft body. The present invention updates the self-adaptive control parameters in real time by introducing the secondary difference of the sailboard deformation displacement and the cumulative amount of the sailboard deformation displacement. The active vibration control method of panel mode estimation also avoids the information loss caused by mode truncation, and realizes the high-precision attitude control of the spacecraft body under the flexible vibration of the sail panel.

[0023] Such as figure 1 Shown is the flowchart of the method of the present invention. Specific steps are as follows:

[0024] (1) Through the binocular measurement algorithm based on the CCD optical imaging sensor, the deformation and displacement of the sailboard root, sailboard middle position, and sailboard end at the cur...