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TECHNOLOGY PREDEVELOPMENT FOR ACTIVE CONTROL OF VIBRATION VERY HIGH ACCURACY POINTING SYSTEMS

机译:主动控制振动和超高精度定位系统的技术预开发

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This paper presents the development of key technologies for the control of micro-vibrations onboard high pointing accuracy satellites. They include the development and/or the pre-qualification of four flight prototypes: 1. The Multi-purpose Active Isolation System (MAIS) is a 6 DOF isolator based on six active struts implemented in an hexapod configuration. It is controlled by an hybrid analogueumerical electronics based on an MCM 21020 DSP board. The MAIS concept covers a large range of applications: isolation of optical payload, reaction wheels, etc. The reference application for the MAIS pre-development is the isolation of a laser diode implemented at the entrance of a telescope to generate a pseudo-star with a pointing stability of 100 nano-radians. 2. The Adaptive Centralised Control System (ACCS) aims at cancelling the disturbances generated by noisy equipment such as reaction wheels at the location of sensitive payloads. The centralised electronics controls acquire the signal of distributed sensors to drive a set of actuators. The objective is to reduce by 30 to 40 dB the effect of harmonic disturbances on the payload by applying destructive vibrations. The ACCS fast signal processing tasks and slow control algorithms are implemented on a MCM 21020 DSP board. 3. An hybrid numeric/analogue electronics board based on a MCM 21020 DSP is developed to acquire the signal of 6 piezo sensors and to drive up to 6 piezo actuators. This board will be used to implement the ACCS function and to drive the MAIS in closed loop at 10 kHz. 4. The Integrated Active Damping Device (IADD) is as a stand-alone device integrating all functions necessary for active damping: piezo sensor & actuator, acquisition, drive & processing electronics. The objective is to define a versatile product applicable to a wide range of space structures at a minimum cost, mass, volume and power consumption. The performance objective is to reduce vibrations by 20 dB at a given frequency.
机译:本文介绍了用于控制高指向精度卫星上的微振动的关键技术的发展。它们包括四个飞行原型的开发和/或资格预审:1.多功能主动隔离系统(MAIS)是基于六脚架配置的六个主动支柱的6自由度隔离器。它由基于MCM 21020 DSP板的混合模拟/数字电子设备控制。 MAIS概念涵盖了广泛的应用范围:光学有效载荷,反作用轮等的隔离。MAIS预先开发的参考应用是在望远镜入口处实现的激光二极管的隔离,以产生伪星。 100纳米弧度的指向稳定性。 2.自适应集中控制系统(ACCS)旨在消除由敏感设备有效位置处的反作用轮等嘈杂设备产生的干扰。集中式电子控件获取分布式传感器的信号以驱动一组执行器。目的是通过施加破坏性振动,将谐波干扰对有效载荷的影响降低30至40 dB。 ACCS快速信号处理任务和慢速控制算法在MCM 21020 DSP板上实现。 3.开发了基于MCM 21020 DSP的混合数字/模拟电子板,以获取6个压电传感器的信号并驱动多达6个压电执行器。该板将用于实现ACCS功能并以10 kHz的闭环驱动MAIS。 4.集成式主动阻尼设备(IADD)是独立的设备,集成了主动阻尼所需的所有功能:压电传感器和执行器,采集,驱动和处理电子设备。目的是定义一种通用产品,以最小的成本,质量,体积和功耗来应用到各种空间结构。性能目标是在给定频率下将振动降低20 dB。

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