Multi-scout point simulation method

Abstract

The invention relates to the technical field of simulation, and discloses a multi-reconnaissance point simulation method. The method includes: S100, judging whether there is a reconnaissance point in the current flight segment, if so, go to S102, otherwise go to S116; S102, based on the theoretical line-of-sight pitch angle and theoretical line-of-sight heading angle of the scout point relative to the aircraft obtained by real-time model solution Calculate the control angle of the turntable; S104, control the two outer frames to move from zero to the predetermined position at a predetermined time interval based on the control angle of the turntable; S106, control the two outer frames to move from the predetermined position to the reconnaissance point based on the theoretical line-of-sight pitch angle and theoretical line-of-sight heading angle Position; S108, judging whether to fly over the reconnaissance point, if it turns to S110, otherwise return to S106; S110, the two outer frames of the control return to zero position from the current position at a predetermined time interval; S112, judging whether there is a next flight segment, if turn to Go to S114, otherwise end; S114, control the aircraft to enter the next segment, return to S100; S116, control the two outer frames to keep zero, return to S112. In this way, the simulation of multiple reconnaissance points can be realized.

Description

technical field [0001] The invention relates to the field of simulation technology, in particular to a multi-reconnaissance point simulation method. Background technique [0002] In hardware-in-the-loop simulation experiments, there is usually only one target point. The guiding device is installed on the inner three frames of the five-axis turntable, and the target simulator is installed on the outer two frames of the five-axis turntable. The attitude of the aircraft is simulated by the inner three frames, and the relative position of the target is simulated by the outer two frames. The movement process of the turntable is controlled by the corresponding data calculated by the simulator software. By controlling the rotation of each frame of the turntable, the relative position change relationship between the guidance device and the target simulator is realized, thereby realizing the simulation for verifying the target recognition ability of the guidance device. [0003] Wi...

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to overcome the deficiencies of the prior art and provide a multi-reconnaissance point simulation method, which can solve the problem that the multi-reconnaissance point cannot be simulated in the above-mentioned prior art

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