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
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[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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