System and method for analyzing influence characteristics of disturbance gravitational field to different forms of ballistic trajectories by using multi-assignment method

A technology of disturbance gravity and characteristic analysis, which is applied in special data processing applications, instruments, electrical digital data processing, etc., and can solve problems such as obvious error accumulation coupling effect and long time affected by disturbance gravity

Active Publication Date: 2017-04-26
黑龙江省工研院资产经营管理有限公司
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Problems solved by technology

At the same time, for long-time low-altitude maneuvering missiles and multi-head guided missiles, etc., they are

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  • System and method for analyzing influence characteristics of disturbance gravitational field to different forms of ballistic trajectories by using multi-assignment method
  • System and method for analyzing influence characteristics of disturbance gravitational field to different forms of ballistic trajectories by using multi-assignment method
  • System and method for analyzing influence characteristics of disturbance gravitational field to different forms of ballistic trajectories by using multi-assignment method

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Embodiment Construction

[0106] The technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0107] refer to figure 2 , the present invention provides a system for analyzing the influence characteristics of a disturbance gravitational field on different forms of ballistics by a multi-assignment method, including a simulation platform main interface module, and the simulation platform main interface module includes a variety of disturbance gravity assignment algorithm selection sub-modules, ballistic form Selection sub-module, analysis sub...

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Abstract

The invention provides a system and method for analyzing the influence characteristics of a disturbance gravitational field to different forms of ballistic trajectories by using a multi-assignment method. The system is constructed based on the idea of modular construction, has high calculation speed and high precision, can adapt to the requirements of analyzing the influence characteristics of disturbance gravitation of different tasks and different forms of ballistic trajectories, and improves the reliability of an analysis result. The system provided by the invention has the advantages of providing a good interactive interface, integrating a general guided missile dynamics model with a disturbance gravitation computing method library, and facilitating the operation and the function expansion of the system.

Description

technical field [0001] The invention relates to a system and method for analyzing the influence characteristics of a disturbance gravitational field on different trajectories by a multi-assignment method. Background technique [0002] The factors that cause the deviation of the missile landing point mainly include the error of the guidance tool and the error of the guidance method. The error of the guidance tool is the deviation of the landing point caused by the imperfect performance of the guidance equipment, such as the inertial platform, accelerometer, gyroscope, and computer, which accounts for about 70% to 80% of the total error. The guidance method error is the landing point deviation caused by the imperfect guidance method. With the improvement of the performance of the guidance equipment, the influence of the guidance method error becomes more and more prominent. Among the factors that cause the error of the guidance method, the disturbance of the gravitational fi...

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Application Information

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IPC IPC(8): G06F17/50
CPCG06F30/23
Inventor 韦常柱常晓华李源丰海何飞毅
Owner 黑龙江省工研院资产经营管理有限公司
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