排序方式: 共有27条查询结果,搜索用时 15 毫秒
1.
改变飞艇重心位置控制纵向运动 总被引:3,自引:0,他引:3
本文针对目前平流层飞艇的运动控制效率较低的问题,重点研究了改变平流层飞艇重心的轴向位置来控制飞艇的纵向运动。首先讨论了考虑飞艇重心位置的力和力矩平衡,并利用德国斯图加特大学风洞试验的数据,进行了算例分析。然后和常用的升降舵控制进行效率比较,得出了在空气密度较低的平流层采用改变重心位置比舵面控制具有优越性的结论。最后提出了改变飞艇重心位置的方法。 相似文献
2.
3.
A Hartmann-Shack wavefront sensor (HSWS) is used in characterization of Hermite-Gaussian beams that are generated from a laser-diode pumped mode generator. By measuring the intensity distribution and the phase gradient distribution of the Hermite-Gaussian beams, we determine the beam width, radius of curvature and M^2factor from the images recorded in the HSWS. The results obtained from the HSWS measurement are compared with the ones obtained from the caustic measurement. 相似文献
4.
5.
研究了LD抽运的单纵模Cr,Tm,Ho∶YAG微片激光器,激光器厚度为1?mm,在用波长785?nm的LD进行端面抽运时,激光器阈值为1060?mW,单纵模激光最大输出功率为31?mW. 对激光器输出功率随温度变化特性进行了研究,验证了CTH∶YAG晶体的温度敏感性. 还研究了激光器的温度调谐特性,实验测得激光器的温度调谐系数为14?GHz/℃.
关键词:
激光光学
CTH∶YAG微片激光器
LD抽运
单纵模运转 相似文献
6.
The twisted Laguerre-Gaussian beam was generated by transforming of Hermite-Gaussian beams through an optical system consisting of three rotated cylindrical lenses. The intensity distribution and phase structure of the twisted hollow beam were theoretically analyzed by using Collins diffraction integral. By utilizing the method of mode decomposition, the theory of transformation was analyzed. In the experiment, micro particles were trapped and rotated by this twisted beam. 相似文献
7.
A high-repetition-rate eye-safe optical parametric oscillator (OPO), using a non-critically phase-matched KTP crystal intracavity pumped by a passively Q-switched Nd:GdVO4/Cr^4+ :YAG laser, is experimentally demonstrated. The conversion efficiency for the average power is 7% from pump diode input to OPO signal output and the slope efficiency is up to 10.3%. With an incident pump power of 7,3 W, the compact intracavity OPO (IOPO) cavity, operating at 15 kHz, produces an average power of 0.57 W at 1570 nm with a pulse width as short as 6 ns. The peak power at 1570 nm is higher than 6.3 kW. 相似文献
8.
9.
阵列半导体激光器的光束参数测量与光纤耦合 总被引:4,自引:0,他引:4
采用ISO推荐的方法测量了发光面为 1μm× 15 0 μm的阵列半导体激光器的光束半径、远场发散角、束腰位置、瑞利长度 ,并根据测量结果计算了光束传输因子 (M2 因子 )。以此为基础 ,研究了半导体激光器光束的快轴准直以及光纤耦合技术 ,采用微柱面透镜准直后 ,阵列半导体激光器快轴方向发散角可减小到 0 .48°。设计了光纤耦合光学系统 ,与 10 0 μm光纤耦合时的耦合效率为 71.0 % ,与 2 0 0 μm光纤耦合时的效率为 83.4%。 相似文献
10.