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Carrier rocket launching support equivalent device and control system

A launch vehicle and simulated launch technology, applied in rocket launchers, offensive equipment, weapon types, etc., can solve the problems of wasting time, increasing research and development funds, and long development process and cycle, saving debugging time, saving research and development funds, The effect of shortening the development cycle

Active Publication Date: 2020-06-16
BEIJING LANDSPACETECH CO LTD
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  • Abstract
  • Description
  • Claims
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Problems solved by technology

During the equipment development process of the "Sanping" test and launch mode, the actual launch vehicle launch support system equipment development process and cycle are very long, and the control system equipment has no actual launch vehicle launch support system equipment during the development process for system debugging and delivery. Acceptance, if the test is carried out on the actual launch support system of the launch vehicle, it will not only waste time but also increase the research and development funds

Method used

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  • Carrier rocket launching support equivalent device and control system
  • Carrier rocket launching support equivalent device and control system

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Embodiment Construction

[0023] The characteristics and exemplary embodiments of various aspects of the present invention will be described in detail below. In order to make the purpose, technical solutions and advantages of the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments. It should be understood that the specific embodiments described here are only configured to explain the present invention and to exemplify the principle of the present invention, and are not configured to limit the present invention. Additionally, the mechanical components in the figures are not necessarily drawn to scale. For example, the size of some structural components or regions in the drawings may be exaggerated for other structural components or regions, so as to facilitate the understanding of the embodiments of the present invention.

[0024] The orientation words appearing in the following description are ...

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Abstract

The invention provides a carrier rocket launching support equivalent device and a control system. The carrier rocket launching support equivalent device comprises a simulating launching platform arranged on at least three movable landing legs and provided with a first dip angle sensor, a simulating erecting arm arranged at one end of the simulating launching platform, hinged through a rotation hinge point and provided with a second dip angle sensor, and a proximity switch simulating plate used for installing proximity switches of the simulating erecting arm, an upper clamp and a windproof device. By application of the carrier rocket launching support equivalent device, the development period can be shortened, the actual debugging time of the carrier rocket launching support system is saved, and meanwhile the development expense is greatly saved.

Description

technical field [0001] The invention relates to the field of carrier rocket launch, in particular to a carrier rocket launch support equivalent device and a control system. Background technique [0002] With the rapid development of my country's aerospace industry, the "three-level" test and launch mode of launch vehicles has gradually emerged. In the equipment development process of the "three-level" test and launch mode, the actual launch vehicle launch support system equipment development process and cycle are very long, and the control system equipment has no actual launch vehicle launch support system equipment during the development process for system debugging and delivery. Acceptance, if the test is carried out on the actual launch vehicle launch support system, it will not only waste time but also increase the research and development funds. [0003] In view of this, it is urgent to design an equivalent device for launch support that avoids a long development cycle...

Claims

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Application Information

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IPC IPC(8): F41F3/04
CPCF41F3/04
Inventor 韦银利吴雪张瑜韩召洋张彦杰杨俊
Owner BEIJING LANDSPACETECH CO LTD
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