Missile load simulation device and method for missile launching vehicle of weapon system

Abstract

The invention provides a missile load simulation device and method for a missile launching vehicle of a weapon system. The missile load simulation device comprises a missile load simulation device host, a single-channel module and a three-channel module, the missile load simulation device host simulates the electrical characteristics of a missile, cooperates with the weapon system firepower control system and the missile launching vehicle launching control system to complete the launching process, and returns corresponding signals. The single-channel module simulates a power supply rated load and an ignition load of a single missile; the three-channel module simulates power supply rated loads and ignition loads of three missiles, and transmits data to the missile load simulation device host through CAN communication for data display, storage and playback. According to the invention, the monitoring, analysis, storage and playback of the power supply performance of the missile launching vehicle of the weapon system under different load capacities are realized, the accuracy is high, and the power supply quality of the power supply module under the on-load condition is ensured.

Description

technical field [0001] The invention relates to the technical field of missile simulation launch of precision guidance weapon system, in particular to a missile load simulation device and method for a missile launch vehicle of a weapon system. Background technique [0002] The weapon system missile launch vehicle is a launch platform for precision-guided munitions. During the combat process, according to the instructions and information of the fire control system, the power-on management, launch preparation, parameter binding, and missile launch functions of the precision-guided munitions are automatically completed. The function and performance of the missile launch vehicle is an important prerequisite for the stable operation of the missile, and it is also an important prerequisite for the weapon system to launch multiple missiles at the same time to intercept the target. [0003] Patent document CN103925852A (application number: CN201410114993.5) discloses a device for si...

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Problems solved by technology

[0005] The shortcomings of the above methods are: the first method cannot simulate the actual load to test the power supply module, it can only detect that the function of the transmission path is intact, and cannot identify the performance of the power supply module of the launch vehicle; the second method can simulate to a certain extent Missile load, but there is a problem that the accuracy cannot be confirmed. When the power supply module is within the target range but is about to collapse, this method is also unpredictable

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