The Spacecraft Sensor Bus as a Means of Harness Reduction

机译：航天器传感器总线是减少线束的一种手段

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《DASIA 2003 》|2003年|1-9|共9页
会议地点 Prague(CZ);Prague(CZ)
作者
Chris Plummer-Cotectic Ltd; Patrick Planck-ESTEC;
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作者单位

Dolf Ledellaan 7, B-3090 Overijse, Belgium, +32 2 6753499, c.plummer@skynet.be;

Keplerlaan 1, 2200AG Noordwijk, The Netherlands, +31 71 565 3692, Patrick.Planck@esa.int;

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原文格式 PDF
正文语种 eng
中图分类航天（宇宙航行） ;
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专利

1. Robustness of System Equivalent Reduction Expansion Process on Spacecraft Structure Model Validation [J] . K. K. Sairajan, G. S. Aglietti AIAA Journal . 2012 ,第11期

机译：系统等效折减展开过程在航天器结构模型验证中的鲁棒性
2. Robust Adaptive Attitude Tracking Control With L2-Gain Performance and Vibration Reduction of an Orbiting Flexible Spacecraft [J] . Qinglei Hu Journal of Dynamic Systems, Measurement, and Control . 2011 ,第1期

机译：具有L2增益性能和减震特性的鲁棒自适应姿态跟踪控制
3. Robust Adaptive Attitude Tracking Control With L_2-Gain Performance and Vibration Reduction of an Orbiting Flexible Spacecraft [J] . Qinglei Hu Journal of Dynamic Systems, Measurement, and Control . 2011 ,第1期

机译：具有L_2增益性能和减震特性的鲁棒自适应姿态跟踪控制
4. The Spacecraft Sensor Bus as a Means of Harness Reduction [C] . Data Systems in aerospace . 2003

机译：航天器传感器总线作为线束减少的手段
5. An IMU-based spacecraft navigation architecture using a robust multi-sensor fault detection scheme. [D] . Haberberger, Samuel J. 2016

机译：使用强大的多传感器故障检测方案的基于IMU的航天器导航架构。
6. A Strap-Down Inertial Navigation/Spectrum Red-Shift/Star Sensor (SINS/SRS/SS) Autonomous Integrated System for Spacecraft Navigation [O] . Zhaohui Gao, Dejun Mu, Yongmin Zhong, 2018

机译：航天器导航的捷联惯性导航/光谱红移/恒星传感器（SINS / SRS / SS）自主集成系统
7. Robustness of System Equivalent Reduction Expansion Process on Spacecraft Structure Model Validation [O] . Sairajan, KK, Aglietti, GS 2012

机译：系统等效折减展开过程在航天器结构模型验证中的鲁棒性
8. A STUDY OF THE EFFECTIVENESS OF VARIOUS METHODS OF VIBRATION REDUCTION ON SIMPLIFIED SCALE MODELS OF THE NIMBUS SPACECRAFT [R] . Huey D. Carden, Robert W. Herr 1964

机译：各种减振方法对NImBUs航天器简化尺度模型的影响研究

The Spacecraft Sensor Bus as a Means of Harness Reduction

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