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Cooperative guidance method for heterogeneous aircraft considering attack time and attack angle constraints

An aircraft and angle technology, which is applied in vehicle position/route/altitude control, instruments, navigation calculation tools, etc., can solve the problem of lack of research on cooperative guidance methods of heterogeneous aircraft, weak information sharing and coordination capabilities, and no information interaction, etc. question

Active Publication Date: 2021-06-04
BEIHANG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] However, most of the existing cooperative guidance methods focus on the design of homogeneous aircraft groups, and there is still little research on the cooperative guidance methods for heterogeneous aircraft
In addition, for multiple aircraft to attack targets at designated time, the existing guidance method is to assign the same attack time command to each aircraft, requiring each aircraft to have the ability to receive attack commands, and there is no information interaction between aircraft, the guidance law Independent design, so the ability of information sharing and coordination is weak

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  • Cooperative guidance method for heterogeneous aircraft considering attack time and attack angle constraints
  • Cooperative guidance method for heterogeneous aircraft considering attack time and attack angle constraints
  • Cooperative guidance method for heterogeneous aircraft considering attack time and attack angle constraints

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Embodiment Construction

[0049] In order to make the object, technical solution and advantages of the present invention clearer, refer to the attached figure 1-4 further illustrate the present invention.

[0050] The inventive cooperative guidance method for heterogeneous aircrafts controlled by attack time includes the following steps:

[0051] Step 1: Establish the mathematical model of the aircraft and the relative motion relationship

[0052] The motion relationship of the main aircraft relative to the target can be expressed as:

[0053]

[0054] where r 0 is the distance between the main aircraft and the target, V 0 represents the constant main vehicle speed, θ 0 The line-of-sight angle of the main aircraft relative to the target, γ 0 Main aircraft track angle, φ 0 Lead angle of main aircraft, normal angular velocity a 0 perpendicular to the direction of velocity.

[0055] The relative motion relationship of the aircraft relative to the target can be expressed as:

[0056]

[0057...

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Abstract

The present invention provides a cooperative guidance method for heterogeneous aircraft considering the constraints of attack time and attack angle, including the following steps: Step 1: Establishing a mathematical model of the aircraft and relative motion relationships; Step 2: Designing a designated time hit guidance law for the main aircraft; Step 3: From the design of aircraft guidance laws. Among them, the aircraft group consists of a single master aircraft and multiple slave aircraft, and only the master aircraft can receive the attack time command. This method first establishes the mathematical model of the master aircraft and the slave aircraft, and gives the motion relationship between the master aircraft and the slave aircraft relative to the target. On this basis, the guidance law for the master aircraft to hit the target at a specified time is designed; Simultaneously with the main aircraft hitting the target, the coordinated guidance law is designed to make the distance between the slave aircraft and the target and the main aircraft and the target consistent, and the line-of-sight angle of the slave aircraft relative to the target tends to the preset desired angle.

Description

technical field [0001] The invention relates to a cooperative guidance method for heterogeneous aircrafts considering attack time and attack angle constraints, which belongs to the field of aircraft guidance and control, and specifically designs a cooperative guidance strategy to realize that the entire group of heterogeneous aircrafts hits a target at a specified time at the same time. Background technique [0002] In military operations, high-value targets are usually protected by defense systems. Therefore, using a single aircraft to independently guide such targets is easily intercepted by the defense system, and the combat success rate is low. Multi-aircraft cooperative guidance is regarded as one of the effective ways to break through the defense system to strike targets, and it is an important direction to realize the transformation from a "platform-centric" single aircraft combat method to a "network-centric" multi-aircraft combat method. Through coordinated operatio...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01C21/20G05D1/10
CPCG01C21/20G05D1/104
Inventor 吕金虎李国飞刘克新朱国梁
Owner BEIHANG UNIV