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排序方式: 共有178条查询结果,搜索用时 31 毫秒
81.
基于神经网络的加速度计静态误差系数标定 总被引:3,自引:0,他引:3
利用具有强自学习性、自适应能力及非线性变换特性的神经网络方法,构造加速度计静态函数型神经网络模型,并用于对加速度计静态误差系数的标定。试验证明,利用该方法标定的系数结果具有高精度性,可较好地满足加速度计误差补偿的要求。 相似文献
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Benjamin Lenoir Bruno Christophe Serge Reynaud 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
The Gravity Advanced Package is an instrument composed of an electrostatic accelerometer called MicroSTAR and a rotating platform called Bias Rejection System. It aims at measuring with no bias the non-gravitational acceleration of a spacecraft. It is envisioned to be embarked on an interplanetary spacecraft as a tool to test the laws of gravitation. 相似文献
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F. Liorzou D. Boulanger M. Rodrigues P. Touboul H. Selig 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2014
The MICROSCOPE mission is fully dedicated to the in-orbit test of the Universality of free fall, the so-called Weak Equivalence Principle (WEP), with an expected accuracy better than 10−15. The test principle consists in comparing the accelerations of two proof masses of different composition in the Earth gravitational field. The payload embarks two pairs of test-masses made of Platinum Rhodium and Titanium alloys at the core of two dedicated coaxial electrostatic accelerometers. These instruments are under qualification for a launch in 2016. 相似文献
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Petro Abrykosov Roland Pail Thomas Gruber Nassim Zahzam Alexandre Bresson Emilie Hardy Bruno Christophe Yannick Bidel Olivier Carraz Christian Siemes 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2019,63(10):3235-3248
The state-of-the-art electrostatic accelerometers (EA) used for the retrieval of non-gravitational forces acting on a satellite constitute a core component of every dedicated gravity field mission. However, due to their difficult-to-control thermal drift in the low observation frequencies, they are also one of the most limiting factors of the achievable performance of gravity recovery. Recently, a hybrid accelerometer consisting of a regular EA and a novel cold atom interferometer (CAI) that features a time-invariant observation stability and constantly recalibrates the EA has been developed in order to remedy this major drawback. In this paper we aim to assess the value of the hybrid accelerometer for gravity field retrieval in the context of GRACE-type and Bender-type missions by means of numerical closed-loop simulations where possible noise specifications of the novel instrument are considered and different components of the Earth’s gravity field signal are added subsequently. It is shown that the quality of the gravity field solutions is mainly dependent on the CAI’s measurement accuracy. While a low CAI performance (10?8 to 10?9?m/s2/Hz1/2) does not lead to any gains compared to a stand-alone EA, a sufficiently high one (10?11?m/s2/Hz1/2) may improve the retrieval performance by over one order of magnitude. We also show that improvements which are limited to low-frequency observations may even propagate into high spherical harmonic degrees. Further, the accelerometer performance seems to play a less prominent role if the overall observation geometry is improved as it is the case for a Bender-type mission. The impact of the accelerometer measurements diminishes further when temporal variations of the gravity field are introduced, pointing out the need for proper de-aliasing techniques. An additional study reveals that the hybrid accelerometer is – contrary to a stand-alone EA – widely unaffected by scale factor instabilities. 相似文献
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本综述将静电悬浮加速度计性能指标项目归为五类,阐述了它们与需求的关系,强调了采样率为10SPS、相应的闭环传递函数带宽为3Hz的必要性。指出实验室标定会受到环境振动噪声的干扰,通常的标定方法均不适用,静态标定的首要困难在于准确测定失准角;用专用摆台作动态标定可以大致判断标度因数并观察两台加速度计模型方程各参数的一致性;为了在专用摆台上进行各项性能测试,加速度计检验质量需要在地面重力下悬浮;落塔试验的功用有限,并非加速度计性能指标的量化评定试验;射前检验加速度计噪声采用分析证实的方法,为了降低噪声,必须依靠详尽的理论分析和实验验证,一一找出各种影响因素及其影响程度,采取有力措施,切实加以改进。
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静电悬浮加速度计伺服控制分析 总被引:2,自引:0,他引:2
根据广义相对论原理选定的坐标系参照物为理想情况下在轨道上自由飘浮的卫星, 据此讨论静电悬浮加速度计检验质量块的运动和电极笼的运动, 得到检验质量在电极内运动的动力学方程, 证明以往相关文献提供的公式存在明显缺陷; 在此基础上分析了伺服控制电路, 给出了电阻尼系数、闭环自然谐振的角频率(或称为加速度计的基础角频率)、受静电负刚度等非受控刚度制约的角频率、来自于静电悬浮的加速度、检验质量的相对位移等一系列表达式, 从而提出必须有足够的增益以提供适度的闭环自然谐振角频率. 给出了位置噪声引起的加速度噪声表达式, 证明当伺服回路的增益足够大时, 在悬浮频带内检验质量的相对位移几乎为零. 相似文献