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本文描述的试制计划,是海军激光陀螺技术的探索性研制工作和激光陀螺制导与导航两个原型系统非常成功的飞行试验演示的结果。此两系统是海军研制的“先进战术惯性制导系统”和霍尼韦尔公司在内部发展资金下研制的“激光惯性导航系统”。对先进战术惯性制导系统和激光惯性导航系统的试验性硬件所做的试验和鉴定,证实了今日的激光陀螺捷联技术具有满足中等质量惯性导航系统基本性能要求的能力。在环形激光陀螺导航仪试制计划中,对单组件激光陀螺导航仪(包括激光陀螺加速表、计算机和电源)进行了研制,以评定其低寿命周期成本可能性、可靠性、可维修性、和在全军事环境下的各种性能因素。这不仅包括陆基的、固定翼和转动翼的飞机环境,而且包括海基的飞机环境,以及环形激光陀螺导航仪与运载工具运动环境相匹配的能力。环形激光陀螺导航仪试制计划所提供的数据,将构成进行施工和试制的研究方案的依据,该方案将提供成本效率高的激光陀螺惯性导航系统以满足范围宽广的未来的武器系统的要求。
The pilot project described in this article is the result of a pilot demonstration of the successful development of naval laser gyro technology and the successful demonstration of two prototype systems of laser gyro guidance and navigation. The two systems are developed by the Navy “advanced tactical inertial guidance system ” and Honeywell “laser inertial navigation system ” developed under the internal development funds. Experiments and evaluations of experimental hardware for advanced tactical inertial guidance systems and laser inertial navigation systems confirm the ability of today’s laser gyro strapdown technology to meet the basic performance requirements of mid-range inertial navigation systems. In the pilot program of the ring laser gyro navigator, a single-component laser gyro navigator (including a laser gyro accelerometer, a computer and a power supply) was developed to assess its low life-cycle cost potential, reliability, maintainability, and Various performance factors under the all-military environment. This includes not only land-based, fixed wing and rotating wing aircraft environments, but also sea-based aircraft environments and the ability of the ring laser gyro navigator to match the vehicle’s movement environment. The data provided by the pilot program of the ring laser gyro navigator will form the basis for a research program on construction and trial production which will provide a cost-effective laser gyro inertial navigation system to meet the requirements of a wide range of future weapon systems.