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Multi-missile cooperative guidance law design method for maneuvering target and time delay communication

A technology of maneuvering targets and design methods, applied in the general control system, adaptive control, control/adjustment system, etc., can solve the problems of missile hit time error, not seen, and reduce the effect of coordinated attack

Active Publication Date: 2019-11-05
SOUTHEAST UNIV
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  • Abstract
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  • Claims
  • Application Information

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Problems solved by technology

Communication time lag may lead to obvious errors in the missile's hit time, reducing the effect of coordinated attacks, so this factor cannot be ignored
For the research on the three-dimensional cooperative guidance law of maneuvering targets under the communication delay, there is no relevant literature

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  • Multi-missile cooperative guidance law design method for maneuvering target and time delay communication
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  • Multi-missile cooperative guidance law design method for maneuvering target and time delay communication

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Embodiment Construction

[0066] The purpose of the invention, technical solutions and advantages of the invention will be described in further detail below in conjunction with the accompanying drawings.

[0067] The existing multi-missile cooperative guidance law, most of the guided missile flight trajectories are in the two-dimensional plane, which cannot describe the flight path of the missile well; in order to achieve the simultaneous attack on the target, the existing guidance law requires the quality of the communication between the missiles. It has very high requirements, which are often impossible to meet in the actual combat environment. If discontinuous control is used in the guidance law, chattering and sudden changes in control input will easily occur, which will greatly damage the missile's engine and steering system and reduce the effect of coordinated attack.

[0068] Based on the above considerations, the present invention first establishes the kinematics model of missiles in three-dime...

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Abstract

The invention discloses a multi-missile cooperative guidance law design method for a maneuvering target and time delay communication. The method includes the steps of, for the maneuvering target whoseacceleration is unknown, establishing a kinematic model of the relative positional relationship between missiles and the target in a three-dimensional space; in a pitch direction and an offset direction, establishing a guidance law by using discontinuous control so that the components, in the two directions, of the relative velocities of the missiles and the target can converge to zero in a limited time and it can be ensured that the missiles can finally hit the target; in the direction of the line of sight, establishing a distributed guidance law by using a communication network between themissiles, a coherence protocol and the discontinuous control so that when the communication network contains time lag, the components of the distance and speed of each missile relative to the target in the direction of the line of sight can be consistent. By using a continuous method and a parameter adaptive method, the guidance law is improved in the three directions, so that control input abruptand buffeting phenomena are reduced while the precision requirement is met.

Description

technical field [0001] The invention relates to a distributed guidance law design method for controlling multiple missiles in coordinated operations in three-dimensional space, in particular to a multi-missile coordinated guidance law design method for maneuvering targets and time-delay communication. Background technique [0002] With the extensive application of new advanced weapons, the air defense early warning mechanism is becoming more and more mature, and the traditional single combat missile has a high probability of being intercepted by the enemy's air defense system, making it difficult to effectively strike the target; while a saturation attack relying on multiple missiles will lead to The cost of attack is too high, reducing the profit of attack. In recent years, communication technology has developed rapidly. Using network information interaction, multi-missiles can achieve coordinated operations and simultaneous strikes on targets, which greatly makes up for th...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B13/04
CPCG05B13/042
Inventor 刘照辉温广辉吕跃祖周佳玲付俊杰
Owner SOUTHEAST UNIV