Six-degree-of-freedom non-decoupling mechanism tail end pose error compensating method in time-varying temperature field

An error compensation and temperature field technology, which is applied in the field of 6-DOF non-decoupling mechanism end pose error compensation method, which can solve the problems of data sensitivity, errors, and affecting the initial position of the center point of the external object.

Active Publication Date: 2017-06-06
LASER FUSION RES CENT CHINA ACAD OF ENG PHYSICS +1
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Problems solved by technology

According to the principle of thermal expansion and contraction, this will cause slight changes in the central point of the external storage at different temperatures, which will directly affect the initial po

Method used

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  • Six-degree-of-freedom non-decoupling mechanism tail end pose error compensating method in time-varying temperature field
  • Six-degree-of-freedom non-decoupling mechanism tail end pose error compensating method in time-varying temperature field
  • Six-degree-of-freedom non-decoupling mechanism tail end pose error compensating method in time-varying temperature field

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Embodiment Construction

[0018] The following description serves to disclose the present invention to enable those skilled in the art to carry out the present invention. The preferred embodiments described below are only examples, and those skilled in the art can devise other obvious variations. The basic principles of the present invention defined in the following description can be applied to other embodiments, variations, improvements, equivalents and other technical solutions without departing from the spirit and scope of the present invention.

[0019] Such as figure 1 As shown, a six-degree-of-freedom non-decoupling mechanism includes a base 1, a Z-direction motion mechanism 2, a yaw motion mechanism 3, a Y-direction motion mechanism 4, an X-direction motion mechanism 5, and a pitch motion mechanism 6 , a scimitar movement mechanism 7 and a tail strut 8, wherein the base 1, the Z-direction movement mechanism 2, the yaw movement mechanism 3, the Y-direction movement mechanism 4, the X-direction ...

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Abstract

A six-degree-of-freedom non-decoupling mechanism tail end pose error compensating method in a time-varying temperature field is provided. The method comprises steps of: establishing a deformation error database related to an external object; determining the actual position of the tail end of the external object after the temperature of the temperature field changes; comparing the actual position and the ideal position of the tail end of the external object to determine the positional deviation value of the tail end of the external object; determining an adjusted value required to be adjusted of the position of the tail end of the external object according to the deviation value of the external object and the deformation error database; and adjusting the position of the tail end of the external object by using the six-degree-of-freedom non-decoupling mechanism according to the adjusted value required to be adjusted of the position of the tail end of the external object. The compensation of the micro change of the position of the tail end of the six-degree-of-freedom non-decoupling mechanism caused by the six-degree-of-freedom non-decoupling mechanism time-varying temperature field external object module error compensation method in a stable inconstant state due to thermal expansion and contraction can improve the motion pose accuracy of the external object.

Description

technical field [0001] The invention relates to an error compensation method, in particular to a method for compensating the end pose error of a six-degree-of-freedom non-decoupling mechanism in a time-varying temperature field. Background technique [0002] The existing industrial and military technology development fields have higher and higher requirements for the spatial motion accuracy of objects, and changes in the ambient temperature will more or less change the original position of the object. Thermal expansion and contraction have a significant impact on occasions that require high position accuracy, so the study of temperature changes on the error compensation of the model has a non-negligible significance. [0003] The wind tunnel is an important technical equipment for aerodynamic research, especially for the development of the country's aerospace industry. If a country wants to develop aircraft and aircraft, it must have a complete set of aerodynamic test facil...

Claims

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Application Information

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IPC IPC(8): G01M9/00G05D1/08
CPCG01M9/00G05D1/0808
Inventor 朱小龙宋代平郑万国谢志江范乃吉袁晓东王凡陈远斌牟力胜
Owner LASER FUSION RES CENT CHINA ACAD OF ENG PHYSICS
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