Inertial pseudo star reference unit

J. Gilmore, T. Chien, R. Wingler
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引用次数: 7

Abstract

Summary form only given. The authors present the development of a precision pointing system, the inertial pseudo-star reference unit (IPSRU). The IPSRU implements a collimated light source mounted on an inertially stabilized platform that is configured using a centrally located two-degree-of-freedom (2-DOF) flexure assembly. The platform inertial sensing is achieved through the combined use of a precision, low-noise 2-DOF dry-tuned rotor gyro (DTG) and two angular displacement sensors (ADS). The composite gyro and ADS implementation optimally combines low-frequency gyro measurements with ADS higher frequency sensing to achieve a composite wide band, extremely low noise, and inertial sensing capability. The collimated light beam in effect becomes a jitter-stabilized pseudo-star. In addition, its pointing direction in inertial space can be changed at a precise rate by commands applied via torquing signals to the gyro.<>
惯性伪星参考单位
只提供摘要形式。作者介绍了一种精密指向系统——惯性伪星参考单元(IPSRU)的研制。IPSRU实现了一个安装在惯性稳定平台上的准直光源,该平台使用中央位置的两自由度(2-DOF)柔性组件进行配置。该平台的惯性传感是通过结合使用一个精密、低噪声的2自由度干调谐转子陀螺(DTG)和两个角位移传感器(ADS)来实现的。复合陀螺仪和ADS实现了低频陀螺仪测量与ADS高频传感的最佳结合,实现了复合宽带、极低噪声和惯性传感能力。准直的光束实际上变成了一个抖动稳定的伪星。此外,它在惯性空间中的指向方向可以通过向陀螺施加扭矩信号的命令以精确的速率改变。
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