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
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[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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