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Multi-missile cooperative guidance method and system under time-varying delay condition

A multi-missile and missile technology, applied to self-propelled missiles, projectiles, offensive equipment, etc., can solve problems such as harsh conditions

Active Publication Date: 2020-09-25
BEIHANG UNIV
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  • Claims
  • Application Information

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Problems solved by technology

In addition, time delay is common and unavoidable in actual physical systems, and multi-bomb cluster systems are no exception, and in complex combat environments, the conditions are often more stringent

Method used

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  • Multi-missile cooperative guidance method and system under time-varying delay condition

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Embodiment Construction

[0069] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. 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.

[0070] In order to make the above objects, features and advantages of the present invention more comprehensible, the present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0071] figure 1 It is a flow chart of a multi-missile cooperative guidance method under the time-varying delay condition provided by the embodiment of the present invention.

[0072] see figure 1 , the multi-mis...

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Abstract

The invention discloses a multi-missile cooperative guidance method and system under a time-varying delay condition. The multi-missile cooperative guidance method under the time-varying delay condition comprises the steps that missile-target motion information is acquired; a missile-target relative motion equation is constructed according to the missile-target motion information; the missile-target relative motion equation is processed by adopting a feedback linearization method to obtain a multi-missile system linear model; and based on a consistency principle, a first normal overload required by the missile and a second normal overload required by the missile are determined according to the multi-missile system linear model, the communication topology function, the communication delay and the missile-target motion information; and the first normal overload and the second normal overload control a plurality of missiles to attack the attack target. Under the condition that time delay exists, the requirement for missile-borne detection equipment can be lowered, and the autonomous performance of the system is improved.

Description

technical field [0001] The invention relates to the field of missile guidance and control, in particular to a multi-missile cooperative guidance method and system under time-varying delay conditions. Background technique [0002] Coordinated guidance of multiple missiles is a hot issue in the field of guidance and control in recent years. Its time-consistent saturation attack on stationary targets or low-speed targets can effectively target enemy radar detection, thereby improving damage capabilities. [0003] There are mainly two types of existing multi-bomb coordination methods. One is to estimate the remaining attack time of missiles. At present, there are several research results on time estimation methods. Among them, the proportional guidance method is used, which leads to the classic time estimation formula. The modulo control method gives the time estimation method and so on. The other is to designate the attack time for coordinated strikes. Each missile calculates...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F42B15/01
CPCF42B15/01
Inventor 董希旺周思全任章李清东韩亮吕金虎
Owner BEIHANG UNIV
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