航空兵器
航空兵器
항공병기
Aero Weaponry
2015年
5期
41-45
,共5页
史要涛%王玉雷%解放%薛文慧%范志刚
史要濤%王玉雷%解放%薛文慧%範誌剛
사요도%왕옥뢰%해방%설문혜%범지강
光学设计%气动光学%非均匀光学介质%像质评估
光學設計%氣動光學%非均勻光學介質%像質評估
광학설계%기동광학%비균균광학개질%상질평고
optical design%aero-optic%inhomogeneous optical medium%image quality assessment
高速气动热环境下,光学头罩会产生无规则非均匀的温度分布和表面变形, 从而给光学成像系统带来严重的成像失真和像偏移. 本文使用有限元分析软件来仿真高速气动热环境,得到光学头罩的温度分布和表面变形,根据热光效应得到折射率分布,使用Code V的自定义面型和梯度折射率来进行光线追迹. 高速光学球头罩的仿真实例表明高速气动热环境下成像失真严重的主要因素是非均匀的头罩折射率分布,而微小的头罩表面形变带来的影响很小.
高速氣動熱環境下,光學頭罩會產生無規則非均勻的溫度分佈和錶麵變形, 從而給光學成像繫統帶來嚴重的成像失真和像偏移. 本文使用有限元分析軟件來倣真高速氣動熱環境,得到光學頭罩的溫度分佈和錶麵變形,根據熱光效應得到摺射率分佈,使用Code V的自定義麵型和梯度摺射率來進行光線追跡. 高速光學毬頭罩的倣真實例錶明高速氣動熱環境下成像失真嚴重的主要因素是非均勻的頭罩摺射率分佈,而微小的頭罩錶麵形變帶來的影響很小.
고속기동열배경하,광학두조회산생무규칙비균균적온도분포화표면변형, 종이급광학성상계통대래엄중적성상실진화상편이. 본문사용유한원분석연건래방진고속기동열배경,득도광학두조적온도분포화표면변형,근거열광효응득도절사솔분포,사용Code V적자정의면형화제도절사솔래진행광선추적. 고속광학구두조적방진실례표명고속기동열배경하성상실진엄중적주요인소시비균균적두조절사솔분포,이미소적두조표면형변대래적영향흔소.
Under high-speed aero-dynamic heating environment, the optical dome will produce an ir-regular and inhomogeneous temperature distribution and surface deformation,resulting in a serious image distortion and image shift to the optical imaging system.In this paper, the finite element analysis software is used to simulate the high-speed aero-dynamic heating environment and then the temperature distribution and surface deformation of the optical dome are got.According to thermo-optic effect, refractive index dis-tribution is got, and"User-Defined Surface" and "User-Defined Gradient Index"of Code V are used for ray tracing.The simulation example of high-speed optical dome indicates that the main factor for serious image distortion under high-speed aero-dynamic thermal environment lies in the inhomogeneous dome re-fractive index distribution, while the tiny surface deformation of dome has little effect on this.