Semi-physical real-time simulation system of laser guided missile
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- 中天长光(青岛)装备科技有限公司
- Publication Date
- 2018-01-19
- Estimated Expiration
- Not applicable · inactive patent
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Abstract
Description
technical field
[0001] The invention relates to laser-guided missiles, and particularly discloses a half-physical real-time simulation system for laser-guided missiles. Background technique
[0002] Laser-guided missiles are launched from fixed-wing aircraft, rotary-wing helicopters or drones. When the ground soldier or aircraft pilot finds the target, the missile and carrier aircraft are notified to enter the ready state. After the missile meets the launch conditions, the missile is launched. At the same time, the ground soldier or carrier aircraft uses the laser irradiator to irradiate the target. After the missile enters the target acquisition area after passing through the initial guidance and intermediate guidance sections, when the missile approaches the target so that the seeker can receive the laser signal reflected from the target, the seeker unlocks and starts to track the target, and the missile enters the final guidance section. And hit the target.
[0003] The...