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Heterogeneous aircraft cooperative guidance method considering attack time and attack angle constraints

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

Active Publication Date: 2020-12-25
BEIHANG UNIV
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  • 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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  • Heterogeneous aircraft cooperative guidance method 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 invention provides a heterogeneous aircraft cooperative guidance method considering attack time and attack angle constraints. The method comprises the following steps of S1, establishing aircraftmathematical models and a relative motion relationship; S2, designing a specified time hit guidance law for a main aircraft; and S3, designing guidance laws for slave aircrafts, wherein the aircraft group is composed of a single main aircraft and a plurality of slave aircrafts, and only the main aircraft can receive an attack time instruction. According to the method, firstly, the mathematical models of the main aircraft and the slave aircrafts are established, a motion relationship between the main aircraft and the slave aircrafts relative to a target is given, and the guide law for hitting the target at a specified moment for the main aircraft is designed on the basis; and in order to ensure that the slave aircrafts and the main aircraft hit the target at the same time, a cooperative guidance law is designed to enable the distance between the slave aircrafts and the target to be consistent with the distance between the master aircraft and the target, and the sight angle of the slaveaircrafts relative to the target tends to a preset expected 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 Applications(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
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