Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

Control system and control method for full-automatic adjustment of rocket perpendicularity

An adjustment method and control system technology, applied to rocket launchers, self-propelled bombs, offensive equipment, etc., can solve problems such as mechanical structure damage, low leveling efficiency, uneven force, etc., to ensure rocket verticality and launch safety Reliable and uniform force on the mechanism

Active Publication Date: 2020-11-17
一重集团(黑龙江)专项装备科技有限公司 +1
View PDF7 Cites 4 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The existing rocket verticality adjustment method is mainly a semi-automatic method, that is, the operator reads the level on the rocket body, reports the value to the console, and then manually calculates the measurement data of the level, and separately adjusts the level of each rocket in the leveling system. The support arm is adjusted to meet the requirements of verticality adjustment, but there are the following problems: first, in the prior art, manual calculation and multiple adjustments rely on personal experience to a certain extent, which is prone to errors and low leveling efficiency; secondly , uneven force tends to occur during the leveling process, causing certain damage to the mechanical structure, thereby increasing the risk of verticality adjustment of the rocket body; moreover, considering the danger of fuel filling, the launch base should be gradually converted to Unattended automatic operation mode minimizes manual participation and improves adjustment efficiency

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Control system and control method for full-automatic adjustment of rocket perpendicularity
  • Control system and control method for full-automatic adjustment of rocket perpendicularity
  • Control system and control method for full-automatic adjustment of rocket perpendicularity

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0034] The specific embodiments of the present invention will be further described below with reference to the accompanying drawings and technical solutions.

[0035]It should be understood that the appended drawings are not to scale, presenting a suitably simplified representation of various features illustrative of the basic principles of the invention. The specific design features of the invention disclosed herein, including, for example, the specific dimensions, orientations, locations, and profiles will be determined in part by the specific intended application and use environment.

[0036] In the accompanying figures, the same or equivalent parts (elements) are referenced with the same reference numerals.

[0037] figure 1 It is a schematic diagram of the installation and connection structure of the support arm and the launch platform in the present invention. see figure 1 , the support arm mechanism 3 is installed on the partition beam of the guide hole of the launch...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

No PUM Login to View More

Abstract

The invention discloses a control system and a control method for full-automatic adjustment of rocket perpendicularity. The control system and the control method for full-automatic adjustment of rocket perpendicularity can automatically and accurately read measurement data of a rocket body gradienter, automatically calculate horizontal data into rocket body perpendicularity parameters, automatically perform numerical calculation and judgment through a support arm controller, distribute different adjustment amounts and adjustment speeds to rocket support arms in different positions, automatically carry out iteration and adjustment actions, and further complete the full-automatic adjustment work of rocket perpendicularity. Compared with existing manual reading and calculation, the control system and control method for full-automatic adjustment of the rocket perpendicularity can automatically and accurately read the measurement data of the rocket body gradienter and further judge whetherthe rocket perpendicularity meets the requirement or not, and an operator can judge whether adjustment needs to be made directly according to the comparison result of the display device.

Description

technical field [0001] The invention belongs to the technical field of rocket launching, and in particular relates to a control system and a control method for fully automatic adjustment of the verticality of a rocket. Background technique [0002] The rocket leveling mechanism generally includes support arms, electrical control systems, servo motors and other components. The number of rocket support arms can be 4, 8 or 12 depending on the rocket model. The specific form is screw-nut transmission mechanism, rocket support arm It is arranged on the upper surface of the launch platform, and there are installation holes on the bottom legs of the rocket. The windproof rod of the rocket support arm passes through the through hole and is fixed by the windproof nut, so as to realize the stable connection between the rocket body and the support arm. [0003] Ideally, after the rocket support arm is installed, the entire automatic leveling mechanism is in a horizontal state, so that ...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
Patent Type & Authority Applications(China)
IPC IPC(8): F42B15/01F41F3/04
CPCF42B15/01F41F3/04Y02P90/02
Inventor 宋永彬杨卓王大鹏刘力改钟国欣张丽静李洪波赵继亮曹斌
Owner 一重集团(黑龙江)专项装备科技有限公司
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products

Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.

© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com