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Space follow-up system

A servo system and space technology, applied in space navigation equipment, simulator of space navigation conditions, transportation and packaging, etc.

Inactive Publication Date: 2013-12-25
ENG DESIGN & RES INST OF GENERAL ARMAMENTS DEPT
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] In the prior art, there is no equipment for flight testing of aircraft in microgravity environment

Method used

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Embodiment Construction

[0092] Such as figure 1 As shown, the space follow-up system of the present invention comprises two vertical supports 37 and a horizontal support 38 fixed on the ground, and the two ends of the horizontal support 38 are respectively fixed on the two vertical supports 37, and on the horizontal support 38 There are two second track beams 14 arranged in parallel along the long side direction of the horizontal bracket 38, a high-speed heavy-duty driving gear synchronous transmission system is arranged above the second track beam 14, and a high-speed heavy-duty driving gear synchronous transmission system is arranged above the high-speed heavy-duty driving gear synchronous transmission system. Vertical follow-up system. The vertical follow-up system is hoisted with a space-floating fast follow-up device through the vertical traction rope 39. A space-following constant tension macro micro-control system is installed below the space-floating fast follow-up device. The space follow-up ...

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Abstract

The invention provides a space follow-up system and relates to equipment for carrying out flight testing on aircrafts in microgravity environment. The invention aims at providing the space follow-up system for carrying out flight testing on aircrafts in the simulated microgravity environment. The space follow-up system comprises two vertical support frames (37) and a horizontal support frame (38), wherein the horizontal support frame is fixedly arranged on the two vertical support frames, two second track beams (14) are arranged on the horizontal support frame, a high-speed heavy load running gear synchronous transmission system is arranged above the second track beams, a vertical follow-up system is arranged above the high-speed heavy load running gear synchronous transmission system, the vertical follow-up system is hoisted with a space floating type fast follow-up device through a vertical traction rope (39), a space follow-up constant tension macro micro control system and a target aircraft (40) are sequentially arranged under the space floating type fast follow-up device, and the space floating type fast follow-up device is connected with six space attitude stabilizing systems through horizontal traction ropes (41).

Description

technical field [0001] The invention relates to a ground test device, in particular to a device for conducting a flight test on an aircraft in a microgravity environment. Background technique [0002] In the prior art, there is no equipment for flight testing the aircraft in a microgravity environment. Contents of the invention [0003] The technical problem to be solved by the present invention is to provide a space follow-up system for flight testing an aircraft in a simulated microgravity environment. [0004] The space follow-up system of the present invention comprises two vertical supports fixed on the ground and a horizontal support, the two ends of the horizontal support are respectively fixed on the two vertical supports, and the horizontal support is provided with The two second track beams are arranged in parallel. The top of the second track beam is equipped with a high-speed heavy-duty driving gear synchronous transmission system. The vertical traction rope ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G7/00
Inventor 万全智浩程刚龚奎成刘建斌王迎东郑志荣常嵩杨元永尚文彭云涛
Owner ENG DESIGN & RES INST OF GENERAL ARMAMENTS DEPT
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