一种基于脉冲宽度的动态补偿方法,用于精确引导飞机中的激光测距和距离确定
Jinghao Li1, Zhipeng Li2, Yuheng He1
1School of Mechanical Engineering, Nanjing University of Science and Technology, Nanjing 210094, China.
Micromachines
|December 31, 2025
概括
本研究引入了激光测距的动态补偿方法,提高了精确引导飞机启动装置的精度. 这种新的方法使用脉冲宽度变化来实现精确的距离测量,平均误差为1.33%.
科学领域:
- 航空航天工程 航空航天工程
- 光学计量学 在光学计量学
- 导航系统 导航系统
背景情况:
- 微型化和高精度对于精确导航飞机的启动装置至关重要.
- 现有的激光测距装置需要提高测量准确度,以便可靠的固定距离启动决策.
- 激光回声特征,特别是回声脉冲宽度变化,冲击距离精度.
研究的目的:
- 开发基于脉冲宽度的激光测距动态补偿方法.
- 为了提高激光测距装置在启动装置系统中的测量精度.
- 确保定距离启动决定在制导飞机中的准确性和可靠性.
主要方法:
- 分析激光回声特征,以了解脉冲宽度变化.
- 建立脉冲宽度和中等范围的检测距离之间的负相关性.
- 实施双校正方法,将静态查找表与动态补偿相结合.
- 开发基于脉冲宽度与距离偏差映射的校准和校正系统.
主要成果:
- 提出并实施了一种动态补偿方法.
- 该方法建立了脉冲宽度和距离偏差之间的映射关系,以进行校正.
- 测试验证了可行性,在计算和实际距离之间实现了小的相对误差.
- 发现平均相对误差大约为1.33%.
结论:
- 提出的动态补偿方法有效地提高了激光测距的精度.
- 这种技术为开发小型化和智能启动设备提供了关键的技术支持.
- 双校正方法可确保精确引导应用程序的可靠距离测量.
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