Onboard comprehensive electronic system

An integrated electronic system and arrow-borne technology, applied in the field of arrow-borne integrated electronic systems, can solve the problems of low reliability of the electrical system, achieve the effects of improving the debugging scheme, reducing weight, and reducing weight and complexity

Pending Publication Date: 2019-12-31
BEIJING XINGJI RONGYAO SPACE TECH CO LTD
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  • Abstract
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Problems solved by technology

[0006] In view of this, the embodiment of the present invention provides an arrow-borne integrated electronic system to solve the problem of low reliability of the existing electrical system

Method used

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Embodiment Construction

[0055] In order to make the purpose, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments It is a part of embodiments of the present invention, but not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those skilled in the art without making creative efforts belong to the protection scope of the present invention.

[0056] It should be noted that the rocket-borne integrated electronic system described in the embodiments of the present invention can be applied in the electrical system of launch vehicles or missile weapons, or in other spacecraft (such as satellites), aircraft integrated electronic systems and high-reliability electronic equipment etc. will be applied...

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Abstract

The invention relates to the technical field of design of onboard electrical systems, in particular to an onboard comprehensive electronic system which comprises at least one function module and a master control module, wherein the function module comprises at least one of a power module, a power distribution module, a timing sequence module, an inertial navigation module and a satellite inertialnavigation; and the master control module is connected with each of the function modules and is used for receiving the data of each function module and processing the data to form corresponding control signals to control a to-be-controlled member. The master control module is cooperated with each function module to form a system meeting different demands; the module dividing manner improves the integration level of the system and also reduces the weight and complexity of the electrical system; the weight of a complete machine is reduced, the integrated design reduces the interconnected cable network among all single machines, and finally, the reliability of the entire electrical system is improved to meet the flight control requirement of the to-be-controlled member.

Description

technical field [0001] The invention relates to the technical field of electrical system design on arrows (bombs), in particular to an arrow-borne integrated electronic system. Background technique [0002] The rocket-borne integrated electronic system is an important core unit of the electrical system of the launch vehicle (or missile weapon), which can realize the guidance control, attitude control, integrated navigation, inertial navigation, satellite navigation, power supply and distribution control, timing control, and autonomous safety of the launch vehicle. With the cooperation of the ground measurement and launch control system, it realizes the control of the arrow test and launch process. [0003] The concept of integrated electronic system comes from the complex electronic system in the aviation field, and is gradually adopted in the aerospace field. Among them, it is first adopted in satellites, which further improves the reliability and integration of satellites...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F42B15/01
CPCF42B15/01
Inventor 江良伟漆光平石翔赵也倪曹扬
Owner BEIJING XINGJI RONGYAO SPACE TECH CO LTD
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