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On-line dynamic balance control method and system for spaceborne rotating camera

A camera and spaceborne technology, applied in the aerospace field, can solve the problems of insufficiency of control accuracy and speed, and complex process.

Active Publication Date: 2019-08-06
HARBIN INST OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Most of the existing dynamic balance control methods are mainly aimed at all kinds of large-scale machinery. They either have complicated processes or the control accuracy and speed cannot meet the requirements of fast dynamic balance for the rotating camera on the planet, especially when the unbalanced vibration signal is weak. Therefore, it is very urgent to develop a dynamic balance control method suitable for this type of rotor to reduce the complexity of the existing dynamic balance realization of the rotating camera, or to improve the accuracy of the technical solution.

Method used

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  • On-line dynamic balance control method and system for spaceborne rotating camera
  • On-line dynamic balance control method and system for spaceborne rotating camera
  • On-line dynamic balance control method and system for spaceborne rotating camera

Examples

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example 1

[0211] This example provides an online dynamic balance control method for a spaceborne rotating camera, which is based on two balance heads that are installed on the left and right end faces of the camera rotor and move in polar coordinates, by driving a total of four balance weights on the two balance heads to rotate in the circumferential direction To achieve the purpose of control, the following steps can be followed:

[0212] Step 1: The balance weight on each balance head does not move, the sensor measures the vibration information of the measuring point, and calculates the first vibration amount at the initial moment They are calculated as

[0213]

[0214] In the formula, X is the vector composed of the vibration amplitude extracted by the vibration sensor at each measuring point, A is the influence coefficient matrix of the unbalance of the correction plane on the test point, m is the mass of the balance weight, and r is the distance between the balance weight and ...

example 2

[0231] Such as Figure 4 As shown, first, the improvement of the technical solution provided by the previous example of this example is explained. Based on two balance heads that move in polar coordinates on the left and right ends of the camera rotor, by driving a total of four balance weights on the two balance heads Circumferential rotation achieves the purpose of control, Figure 4 The middle z-axis is the axial direction of the rotor shaft, the unbalanced mass of the camera rotor is P, and two balance heads are respectively arranged on the left and right end surfaces of the camera rotor (such as Figure 4 As shown, the balance end face 1 and the balance end face 2), each balance head contains two balance weights, and the balance weights move according to polar coordinates. The balance weight can rotate in the circumferential direction on a surface with a radius r from the rotating shaft, and the angular positions of the four balance weights are φ 11 , φ 12 and φ 21 , ...

example 3

[0233] Such as Figure 5 As shown, this example provides an online dynamic balance control method for a spaceborne rotating camera, including:

[0234] S1: Obtain the initial value of the vibration amount (corresponding to the aforementioned first vibration amount) through measurement and calculation;

[0235] S2: Rotate the balance weight for the first time, measure and calculate the vibration amount (corresponding to the aforementioned second vibration amount);

[0236] S3: Calculate the value of the fixed quantity;

[0237] S4: Rotate the balance weight for the second time, measure and calculate the vibration amount (corresponding to the aforementioned third vibration amount);

[0238] S5: Calculate the current angle of the balance weight;

[0239] S6: Calculate the angle required to rotate the balance weight;

[0240] S7: Judging whether the balance requirements are met, if the adjustment is over, if not, go to S8:

[0241] S8: Judging whether the highest precision is...

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Abstract

The invention provides an online dynamic balance control method and system for a spaceborne rotary camera. The method comprises steps that after keeping the present position of a balance head relative to the spaceborne rotary camera, adjusting a relative angle of each balance block of the balance head relative to the spaceborne rotary camera at a first angle, adjusting a relative angle of one balance block of the balance head relative to the spaceborne rotary camera at a second angle and adjusting a relative angle of another balance block of the balance head relative to the spaceborne rotary camera at a third angle, measurement is respectively carried out, and the vibration information corresponding to a movement state of online movement of the spaceborne rotary camera is measured; based on the vibration information, vibration amount and fixing amount corresponding to each piece of vibration information are calculated, lastly, on the condition that an initial angle of the balance block is not clear, adjusting amount of the balance blocks relative to the present angles is simply determined, and online movement of the spaceborne rotary camera is adjusted to reach balance requirement conditions.

Description

technical field [0001] The invention relates to the field of aerospace technology, in particular to an online dynamic balance control method and system for a spaceborne rotating camera. Background technique [0002] The rotating camera is one of the important components of the satellite, and the rotating camera mounted on the satellite is called a spaceborne rotating camera. When the satellite-borne rotating camera is working in orbit, it needs to quickly and accurately take pictures of the target and take pictures, which puts forward high requirements for the balance and stability of the entire satellite and the camera rotor. The mass eccentricity of the satellite-borne rotating camera in the design and assembly process will cause the satellite and the camera to vibrate eccentrically during the in-orbit operation process. Even a very weak vibration will seriously threaten the alignment accuracy of the camera and take pictures. It has an extremely adverse effect on the atti...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01M1/16
CPCG01M1/16
Inventor 曹喜滨孔宪仁李海勤王峰陈雪芹李冬柏
Owner HARBIN INST OF TECH