Relevant bibliographies by topics / Micro-Satellite Attitude Determination

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Book chapters
  4. Conference papers

Academic literature on the topic 'Micro-Satellite Attitude Determination'

Author: Grafiati
Published: 4 June 2021
Last updated: 7 September 2023

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Journal articles on the topic "Micro-Satellite Attitude Determination"

1

Xiu-feng, He, and Ling Keck-voon. "Micro-Satellite Attitude Determination Using GPS Carrier Phases." Wuhan University Journal of Natural Sciences 8, no. 2 (2003): 693–96. http://dx.doi.org/10.1007/bf02899836.

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Ouyang, Gaoxiang, Xin Dong, and Xin Li. "Micro-Satellite Attitude Determination with Only a Single Horizon Sensor." MATEC Web of Conferences 51 (2016): 03008. http://dx.doi.org/10.1051/matecconf/20165103008.

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Cao, Lu, Wei Wei Yang, Xiao Qian Chen, and Yi Yong Huang. "The Research of Micro-Satellite Attitude Determination Based on Predictive Filter." Applied Mechanics and Materials 110-116 (October 2011): 5413–19. http://dx.doi.org/10.4028/www.scientific.net/amm.110-116.5413.

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— An extended predictive filter is presented for attitude determination of Micro-satellite based on the basic theory of predictive filter. This algorithm enhances the precision of kinematics equation, accurately estimates satellite attitude angle and angular velocity using measurement vectors from magnetometer and sun sensors by predicting model errors and angular velocity errors one step ahead. In addition, a new measurement model is derived about angular velocity, which improved the efficiency of the use of measurement vectors. Simulation results show both the high reliability and precision
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Chen, Yajing, Tao Meng, and Zhonghe Jin. "Agile Micro-nano Satellite Attitude Estimation with Lost Measurements." Journal of Physics: Conference Series 2459, no. 1 (2023): 012138. http://dx.doi.org/10.1088/1742-6596/2459/1/012138.

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Abstract Aiming at the problem of lost measurement in attitude determination process of the agile micro-nano satellite, a novel algorithm is proposed employing the Bernoulli process to describe the loss process. Firstly,the model of gyro and star sensors as well as the satellite attitude estimation system simplified with gyro is given. Since the missing observations, the modified EKF algorithm is derived by combining a Bernoulli random variable and a real-time measurement noise correction algorithm. Then the convergence of the improved algorihtm is analyzed, and the bottom boundary condition f
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Shou, Ho-Nien. "Microsatellite Attitude Determination and Control Subsystem Design and Implementation: Software-in-the-Loop Approach." Mathematical Problems in Engineering 2014 (2014): 1–12. http://dx.doi.org/10.1155/2014/904708.

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The paper describes the development of a microsatellite attitude determination and control subsystem (ADCS) and verification of its functionality by software-in-the-loop (SIL) method. The role of ADCS is to provide attitude control functions, including the de-tumbling and stabilizing the satellite angular velocity, and as well as estimating the orbit and attitude information during the satellite operation. In Taiwan, Air Force Institute of Technology (AFIT), dedicating for students to design experimental low earth orbit micro-satellite, called AFITsat. For AFITsat, the operation of the ADCS co
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Zhou, Meng Meng, G. M. Gao, and Hong Bo Yang. "Multi-Source Information Fusion Based on Kalman Filtering." Applied Mechanics and Materials 727-728 (January 2015): 863–66. http://dx.doi.org/10.4028/www.scientific.net/amm.727-728.863.

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Thehigh-frequency angular micro-vibration on satellite platform results in theoptical axis pointing decreasing accuracy. The Kalman filtering based on attitudeinformation fusion method is presented to solve this case and improve the pointing accuracy of attitude determination. Thesimulation results indicate that the estimated accuracy of Kalman filteringattitude information fusion method is better than the result only fromconventional low frequency sensor. Accordingly, the attitude information fusionmethod is verified and accuracy.
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Shou, Ho Nien. "Discoid and Asymmetrical Micro-Satellite Propulsion Mode Attitude Control with Great Mass Change and without Angular Rate Sensor." Applied Mechanics and Materials 479-480 (December 2013): 753–57. http://dx.doi.org/10.4028/www.scientific.net/amm.479-480.753.

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The center of mass of the micro-satellite can offset due to fuel consumption in the course of propulsion, with the interference of external orbital environment such as gravity gradient torque and solar radiation torque. If the structural shape is discoid and asymmetrical, the attitude control may be difficult. The only solution is to design a robust controller, so that the attitude pointing of the satellite can meet the mission requirements with the interference of internal parameter perturbation and external disturbance. This study applied the robust control theory control law in the design o
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Ziebart, Marek, and Paul Cross. "LEO GPS attitude determination algorithm for a micro-satellite using boom-arm deployed antennas." GPS Solutions 6, no. 4 (2003): 242–56. http://dx.doi.org/10.1007/s10291-002-0023-5.

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LE, XUAN HUY, KAZUYA ISHIZAKA, and SABURO MATUNAGA. "H2 A robust attitude determination algorithm based on Unscented Kalman Filter for Micro Satellite." Proceedings of the Space Engineering Conference 2010.19 (2011): _H2–1_—_H2–6_. http://dx.doi.org/10.1299/jsmesec.2010.19._h2-1_.

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ZHANG He, QIN Weiwei, ZHOU Cheng, SONG Hengxin, HUA Yufeng, and WANG Yu. "Attitude Determination Algorithm for Micro-satellite Based on High-order UKF Using Information Fusion." Chinese Journal of Space Science 40, no. 6 (2020): 1091. http://dx.doi.org/10.11728/cjss2020.06.1091.

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Dissertations / Theses on the topic "Micro-Satellite Attitude Determination"

1

Wang, Kuo-Nung, and 汪國農. "Design and Validation of Micro Satellite Attitude Determination and Control Subsystem." Thesis, 2009. http://ndltd.ncl.edu.tw/handle/34005105547012429987.

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碩士<br>國立成功大學<br>電機工程學系碩博士班<br>97<br>The objective of the CKUTEX (Cheng-Kung University Technology Experimental Satellite) micro-satellite project is developing domestic experimental satellite technique. CKUTEX micro satellite will reconstruct the satellite and launcher’s propulsion and control characteristics by using the data collected at the satellite in separation stage including position, velocity, attitude and torque. The thesis describes the design and implementation of the CKUTEX micro-satellite attitude determination and control subsystem and investigates the method to reconstruct traj
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Pal, Madhumita. "Accurate and Efficient Algorithms for Star Sensor Based Micro-Satellite Attitude and Attitude Rate Estimation." Thesis, 2013. http://etd.iisc.ac.in/handle/2005/3428.

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This dissertation addresses novel techniques in determining gyroless micro-satellite attitude and attitude rate. The main objective of this thesis is to explore the possibility of using commercially available low cost micro-light star sensor as a stand-alone sensor for micro-satellite attitude as well as attitude rate determination. The objective is achieved by developing accurate and computationally efficient algorithms for the realization of onboard operation of a low fidelity star sensor. All the algorithms developed here are tested with the measurement noise presented in the catalog of the
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Pal, Madhumita. "Accurate and Efficient Algorithms for Star Sensor Based Micro-Satellite Attitude and Attitude Rate Estimation." Thesis, 2013. http://etd.iisc.ernet.in/2005/3428.

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This dissertation addresses novel techniques in determining gyroless micro-satellite attitude and attitude rate. The main objective of this thesis is to explore the possibility of using commercially available low cost micro-light star sensor as a stand-alone sensor for micro-satellite attitude as well as attitude rate determination. The objective is achieved by developing accurate and computationally efficient algorithms for the realization of onboard operation of a low fidelity star sensor. All the algorithms developed here are tested with the measurement noise presented in the catalog of the
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Book chapters on the topic "Micro-Satellite Attitude Determination"

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"Attitude Determination and Control System of the Micro/Nano Satellite." In Space Microsystems and Micro/nano Satellites. Elsevier, 2018. http://dx.doi.org/10.1016/b978-0-12-812672-1.00003-5.

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Ni, Feng, Haiyang Quan, and Wenjie Li. "Micro-satellite attitude determination based on federated Kalman filter using multiple sensors." In Automotive, Mechanical and Electrical Engineering. CRC Press, 2017. http://dx.doi.org/10.1201/9781315210445-32.

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Ni, Feng, Haiyang Quan, and Wenjie Li. "Micro-satellite attitude determination based on MEKF using MEMS gyroscope and magnetometer." In Automotive, Mechanical and Electrical Engineering. CRC Press, 2017. http://dx.doi.org/10.1201/9781315210445-73.

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Conference papers on the topic "Micro-Satellite Attitude Determination"

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Min Li, Song-yan Wang, Bao-long Zhu, Ying-chun Zhang, and Hua-yi Li. "Micro-satellite attitude determination algorithm based on adaptive UKF." In 2013 International Conference on Mechatronic Sciences, Electric Engineering and Computer (MEC). IEEE, 2013. http://dx.doi.org/10.1109/mec.2013.6885512.

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Shou, Ho-Nien, Jia-Shing Sheu, and Jyh-Haw Wang. "Micro-satellite detumbling mode attitude determination and control : UKF approach." In 2010 8th IEEE International Conference on Control and Automation (ICCA). IEEE, 2010. http://dx.doi.org/10.1109/icca.2010.5524162.

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Shou, Ho-Nien, and Chen-Tsung Lin. "Micro-satellite attitude determination: Using Kalman filtering of magnetometer data approach." In 2010 International Symposium on Computer, Communication, Control and Automation (3CA). IEEE, 2010. http://dx.doi.org/10.1109/3ca.2010.5533589.

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Zhang, Zhen, Jin Jin, and Jianping Xiong. "Research on attitude determination of micro-satellite with impact of remanence." In International Conference on Optical Instruments and Technology (OIT2013), edited by Brian Culshaw, Xuping Zhang, and Anbo Wang. SPIE, 2013. http://dx.doi.org/10.1117/12.2038178.

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Shou, Ho Nien. "Micro-satellite Attitude Determination and Control Subsystem Design and Implementation: Software-in-the-Loop Approach." In 2014 International Symposium on Computer, Consumer and Control (IS3C). IEEE, 2014. http://dx.doi.org/10.1109/is3c.2014.331.

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Cao, Lu, Weiwei Yang, Xiaoqian Chen, and Yiyong Huang. "Application of Multi-Sensors Data Fusion Based on Improved Federal Filtering in Micro-Satellite Attitude Determination." In 2011 International Workshop on Multi-Platform/Multi-Sensor Remote Sensing and Mapping (M2RSM). IEEE, 2011. http://dx.doi.org/10.1109/m2rsm.2011.5697393.

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Fritz, T. A., D. B. Pledger, and T. R. Werner. "Diffractive Optics in an Ultraviolet Satellite Attitude Sensor." In Diffractive Optics and Micro-Optics. Optica Publishing Group, 1996. http://dx.doi.org/10.1364/domo.1996.dthb.5.

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Honeywell's Earth Reference Attitude Determination Sensor (ERADS) is a wide field of view ultraviolet imaging sensor for satellite attitude determination. The sensor was designed for small satellite applications1, where size, weight, and cost are the primary drivers. Use of the ultraviolet region of the spectrum provides a unique capability to simultaneously image stars, Earth's limb (day or night), and other celestial objects, and to tolerate the sun in the field of view. This is because the solar output is lower relative to the other objects of interest in this waveband, and eliminates the n
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