Twelve-degree-of-freedom space simulator butt-joint performance testing device

A test device and simulator technology, which is applied in the field of aerospace ground simulation experiments, can solve problems such as insufficient simulation accuracy of spacecraft, and achieve high-precision and large-scale motion, accurate matching results, and low-mass effects

Active Publication Date: 2018-04-03
SHANGHAI AEROSPACE SYST ENG INST +1
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  • Abstract
  • Description
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  • Application Information

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Problems solved by technology

[0003] The purpose of the present invention is to provide a 12-DOF space simulator docking performance test device to solve the problem that

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  • Twelve-degree-of-freedom space simulator butt-joint performance testing device
  • Twelve-degree-of-freedom space simulator butt-joint performance testing device
  • Twelve-degree-of-freedom space simulator butt-joint performance testing device

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Embodiment Construction

[0045] The 12-DOF aerospace simulator docking performance test device proposed by the present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments. Advantages and features of the present invention will be apparent from the following description and claims. It should be noted that the drawings are all in a very simplified form and use imprecise ratios, which are only used to facilitate and clearly assist the purpose of illustrating the embodiments of the present invention.

[0046] figure 1 Schematic diagram of the structure of the portable feeler gauge automatic online verification device provided by the embodiment of the present invention; figure 2 It is a schematic diagram of the test structure of the base in the portable feeler gauge automatic online verification device provided by the embodiment of the present invention. refer to figure 1 as well as figure 2 , provides a portable automatic online v...

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Abstract

The invention provides a twelve-degree-of-freedom space simulator butt-joint performance testing device. The device includes a two-dimensional horizontal movement driving unit, an active yawing driving unit, a passive yawning driving unit, an active space simulator body and a passive space simulator body; the active and passive yawing driving units are arranged at the two ends of the two-dimensional horizontal movement driving unit respectively, the active space simulator body is arranged on the active yawing driving unit, and the passive space simulator body is arranged on the passive yawingdriving unit; the active yawing driving unit drives the active space simulator body to simulate an active end of a butt-joint mechanism; the passive yawning driving unit and the passive space simulator body simulate a passive end of the butt-joint mechanism. Movement coupling among the degrees of freedom of the space simulator is small, the implementation of each degree of freedom is sensitive andreliable, the movement range is wide, the movement track is not limited, and by adopting an air flotation technique, the simulation precision is high.

Description

technical field [0001] The invention relates to the field of aerospace ground simulation experiments, in particular to a 12-degree-of-freedom aerospace simulator docking performance test device. Background technique [0002] In order to test the docking performance of the third-phase lunar exploration docking and sample transfer subsystem under normal temperature conditions, it is necessary to provide equipment for ground test research and test verification. The equipment needs to have two aerospace simulators with three translational and three rotational degrees of freedom respectively, and at the same time satisfy the simulation of the physical properties of the motion of the real aircraft. However, there is no high-precision aerospace simulator with six degrees of freedom at present. The existing six-degrees of freedom aerospace simulators often use liquid flotation and flexible cable suspension methods. The liquid flotation method can only be suitable for certain aeros...

Claims

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Application Information

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IPC IPC(8): B64G7/00G09B25/02G01M99/00
CPCB64G7/00G01M99/00G09B25/02
Inventor 张玉花徐志刚胡震宇郑云青朱雪龙王治易李洪波俞旦倪波刘洲贺云刘勇
Owner SHANGHAI AEROSPACE SYST ENG INST
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