Laser guidance missile changing laser energy simulation method for unmanned aerial vehicle and system
A laser energy and laser guidance technology, applied in general control systems, control/regulation systems, design optimization/simulation, etc., can solve problems such as the inability to verify the seeker signal fluctuation missile control system, to improve efficiency and accuracy, The effect of reducing the number of target tests in the shooting range and shortening the development progress
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Embodiment 1
[0055] When the UAV launches an airborne laser-guided missile, it first searches, finds and locks the target through the airborne photoelectric reconnaissance load, and then uses the airborne laser irradiator to emit a laser beam to the target, and the laser seeker of the UAV airborne missile passes through the Receive the laser echo diffusely reflected by the target, identify and solve it and lock until it hits the target. Due to the good monochromaticity of the laser and the small beam divergence, it is difficult for the enemy to effectively interfere with the guidance system, and the irradiation accuracy is generally within 1 meter. Therefore, laser-guided weapons attacking fixed or moving targets have advantages that other guidance methods cannot match.
[0056] In the early stage of missile design, in order to speed up the development progress, reduce the development cost, and reduce the number of field target test flights, semi-physical simulation systems are often used t...
Embodiment 2
[0075] The specific embodiment 2 of the present invention will be further described in detail below in conjunction with the accompanying drawings.
[0076] like figure 1 As shown, a variable laser energy simulation method for UAV laser guided missiles is characterized in that:
[0077] In the missile semi-physical simulation system, the variable energy laser target signal simulator U11 is used to simulate the change of the target laser signal received by the laser seeker U12 during the flight of the missile, and the missile flight simulation is carried out;
[0078] The semi-physical simulation system includes a simulation control telemetry system U3, a simulation computer U2, and a five-axis turntable U1;
[0079] The five-axis turntable U1 is divided into three inner axes and two outer axes. The inner three axes are used to simulate the flight attitude of the missile to realize the roll, yaw and pitch motion of the missile; the outer two axes are used to simulate the target...
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