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A distributed control high-precision leveling and erecting control system and method

A distributed control and control system technology, applied in the directions of comprehensive factory control, electrical program control, and comprehensive factory control, etc., can solve the problems of poor mobility, complicated operation, and long time-consuming to erect the launch vehicle, so as to improve the launch maneuverability. The effect of high stability and high control precision

Active Publication Date: 2019-04-05
BEIJING INST OF SPACE LAUNCH TECH +1
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  • Abstract
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Problems solved by technology

[0002] The traditional launching vehicle generally adopts the launching method of fixed platform, which requires a lot of manpower and material support, and has poor maneuverability, low accuracy of launching positioning angle, slow response speed, and complicated operation, especially when the launching vehicle is displayed. It takes a long time to erect, the display efficiency is low, and the user experience is poor

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  • A distributed control high-precision leveling and erecting control system and method
  • A distributed control high-precision leveling and erecting control system and method

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Embodiment Construction

[0027] Such as figure 1 As shown, according to an embodiment of one aspect of the present invention, the present invention provides a distributed control high-precision leveling and erecting control system, including a vehicle control computer, a main control unit, an integrated controller, and multiple bodywork general control units and multiple digital valve control units, the vehicle control computer, main control unit, multiple bodywork general control units and multiple digital valve control units are all connected to each other through the CAN bus for control information, process information, status information and alarm information interaction, the integrated controller is unidirectionally electrically connected to the main control unit through the switching quantity acquisition IO channel of the main control unit, and the main control unit is used to collect control information from the integrated controller and Execute corresponding process control according to the co...

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Abstract

In order to ensure that a launching vehicle control system meets the demand of vehicle control in a mobile environment, the invention provides a distributed control high-precision leveling erection control method and a distributed control high-precision leveling erection control method. The distributed control high-precision leveling erection control method and the distributed control high-precision leveling erection control method can improve the launching maneuverability of launching vehicles, meet the demand for functions like launching vehicle spread, erection, lay-down, support rod folding, aiming window opening and aiming window closing, achieve very high control accuracy, and achieve leveling control precision less than or equal to + / -20'.

Description

technical field [0001] The present invention relates to the technical field of distributed control of electrical buses, and more specifically, to a distributed control high-precision leveling and erecting control system and method. Background technique [0002] The traditional launching vehicle generally adopts the launching method of fixed platform, which requires a lot of manpower and material support, and has poor maneuverability, low accuracy of launching positioning angle, slow response speed, and complicated operation, especially when the launching vehicle is displayed. It takes a long time to erect, the display efficiency is low, and the user experience is poor. [0003] In this context, it is necessary to provide a control system and method for the launching vehicle, so that it can receive the process control of the vehicle control host or collect the process control of the integrated controller button through the CAN bus, so as to realize the launch, erection, lower...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05B19/418H04L12/40
CPCY02P90/02
Inventor 刘杰李向阳刘显勤刘云秋李仁洙程腊腊许进亮苏娟
Owner BEIJING INST OF SPACE LAUNCH TECH