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Necessary and Sufficient Conditions for Attitude Estimation in Fractionated Spacecraft Systems

机译：分式航天器系统中姿态估计的充要条件

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Lars Blackmore; Fred Y. Hadaegh;
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年度 2012
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1. Attitude Estimation in Fractionated Spacecraft Cluster Systems [J] . NASA Tech Briefs . 2011,第1期

机译：航天器集群系统中的姿态估计
2. Recovery of information through linear prediction technique in attitude estimation of spacecraft systems [J] . Khan Naeem, Khan Latif Ullah, Khattak M. Irfan, Measurement . 2015,第Null期

机译：通过线性预测技术恢复航天器姿态估计中的信息
3. A Necessary and Sufficient Condition for Output Feedback Stabilizability: Application for Attitude Control Systems of Micro Satellite. [J] . A.elakkary N.elalami Journal of Theoretical and Applied Information Technology . 2009,第3期

机译：输出反馈稳定性的充要条件：微型卫星姿态控制系统的应用。
4. Necessary and Sufficient Conditions for Attitude Estimation in Fractionated Spacecraft Systems [C] . L. Blackmore, F. Hadaegh AIAA Guidance, Navigation, and Control Conference and Exhibit;AIAA Atmospheric Flight Mechanics Conference;AIAA Modeling and Simulation Technologies Conference . 2009

机译：分式航天器系统中姿态估计的充要条件
5. ATTITUDE DETERMINATION OF A SPINNING SPACECRAFT THROUGH APPLICATION OF DETECTED AND IDENTIFIED STAR TRANSITS TO THE ESTIMATION OF SPACECRAFT MODEL PARAMETERS. [D] . WALSH, THOMAS MICHAEL. 1974

机译：通过将检测到的和确定的恒星变迁应用到空间模型参数的估计中，对纺丝工艺进行姿态确定。
6. Accurate Attitude Estimation Using ARS under Conditions of Vehicle Movement Based on Disturbance Acceleration Adaptive Estimation and Correction [O] . Li Xing, Yijun Hang, Zhi Xiong, 2016

机译：基于扰动加速度自适应估计与校正的车辆运动条件下基于ARS的精确姿态估计
7. Influence estimation of reaction wheel position errors of spacecraft attitude control system on its attitude control accuracy [O] . E.V. Khoroshylov, S.V. Khoroshylov 2005

机译：影响航天器姿态控制系统反应轮定位误差对其姿态控制精度的影响

Necessary and Sufficient Conditions for Attitude Estimation in Fractionated Spacecraft Systems

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