Relevant bibliographies by topics / Magnetorquer

Contents

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

Academic literature on the topic 'Magnetorquer'

Author: Grafiati
Published: 4 June 2021
Last updated: 20 February 2023

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Journal articles on the topic "Magnetorquer"

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Bai, Bo, Jun Zhou, and Shengyun Wang. "Design of High-Performance Magnetorquer with Air Core for CubeSat." Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University 36, no. 1 (2018): 1–6. http://dx.doi.org/10.1051/jnwpu/20183610001.

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To solve the problem that how to design a big magnetic moment, small size, light weight, low power consumption magnetorquer with air core under the constraint of limited volume and power in CubSate, multiobjective optimization design method is used. Firstly, based on the structure of the square support with multiple layer of the enameled wire wrapped, the magnetic moment model, power consumption model and mass model are deduced from square support size, enameled wire diameter and turn number, respectively. Secondly, according to the model of magnetic moment and power consumption, the multi-obj
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Si, Juntian, Yang Gao, and Abadi Chanik. "Slew Control of Prolate Spinners Using Single Magnetorquer." Journal of Guidance, Control, and Dynamics 39, no. 3 (2016): 719–27. http://dx.doi.org/10.2514/1.g001035.

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MIYATA, Kikuko, Tomohiro NARUMI, and Jozef C. van der HA. "Comparison of Different Magnetorquer Control Laws for QSAT." TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, SPACE TECHNOLOGY JAPAN 7, ists26 (2009): Pd_43—Pd_48. http://dx.doi.org/10.2322/tstj.7.pd_43.

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Kuiper, Hans, and Dennis Dolkens. "A cutting edge 6U CubeSat ADCS design for Earth observation with sub-meter spatial resolution at 230–380 km altitude." CEAS Space Journal 12, no. 4 (2020): 613–21. http://dx.doi.org/10.1007/s12567-020-00323-7.

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Abstract A 6U CubeSat for Earth observation in 230–350 km orbits with sub-meter resolution is presented. The proposed Stable and Highly Accurate Pointing Earth-Imager (SHAPE) system’s attitude determination and control system (ADCS) is composed of a single momentum bias wheel with magnetic bearings at rotational speeds of 6000–7000 rpm and refined magnetorquers. Reaction wheels as instability source are absent. The ADCS stabilizes the spacecraft attitude by counteracting the torques from external disturbances in the thermosphere down to < 1° pointing accuracy and < 0.1° instability. The
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Hou, Xu Guang, Jian Yan, Jin Jin, and Shun Liang Mei. "Magnetorquer Based Vertical Damping Method for Microsatellite Attitude Control." Applied Mechanics and Materials 263-266 (December 2012): 584–87. http://dx.doi.org/10.4028/www.scientific.net/amm.263-266.584.

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Aiming at a three-axis stabilized microsatellite, a novel attitude control method, called magnetorquer based vertical damping, is proposed to avoid the occurrence of the worst situation that the non-solar-battery-plane spins towards the sun. DSP based simulation results based on DSP show that the vertical damping method outperforms the simple damping method when no orbit information is available, simultaneously the whole attitude control scheme is simple and effective. The proposed solution guarantees a stable power supply from the electrical source even under the extreme situation, which impr
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Ali, Anwar, Shoaib Ahmed Khan, M. Usman Khan, Haider Ali, M. Rizwan Mughal, and Jaan Praks. "Design of Modular Power Management and Attitude Control Subsystems for a Microsatellite." International Journal of Aerospace Engineering 2018 (December 17, 2018): 1–13. http://dx.doi.org/10.1155/2018/2515036.

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The Electric Power System (EPS) and attitude control system (ACS) are the essential components of any satellite. EPS and ACS efficiency and compactness are substantial for the proper operation and performance of the satellite’s entire mission life. So, realizing the significance of EPS and ACS subsystems for any satellite, they have been assimilated and developed in modular forms focusing on efficiency and compactness. The EPS is comprised of three modules called the solar panel module (SPM), power conditioning module (PCM), and power distribution module (PDM) while the ACS has an embedded mag
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Utama, S., P. R. Hakim, and M. Mukhayadi. "Quarter orbit maneuver using magnetorquer to maintain spacecraft angular momentum." IOP Conference Series: Earth and Environmental Science 284 (May 31, 2019): 012046. http://dx.doi.org/10.1088/1755-1315/284/1/012046.

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Kondo, Kota, Ilya Kolmanovsky, Yasuhiro Yoshimura, Mai Bando, Shuji Nagasaki, and Toshiya Hanada. "Nonlinear Model Predictive Detumbling of Small Satellites with a Single-Axis Magnetorquer." Journal of Guidance, Control, and Dynamics 44, no. 6 (2021): 1211–18. http://dx.doi.org/10.2514/1.g005877.

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Ali, Anwar, M. Rizwan Mughal, Haider Ali, Leonardo M. Reyneri, and M. Naveed Aman. "Design, implementation, and thermal modeling of embedded reconfigurable magnetorquer system for nanosatellites." IEEE Transactions on Aerospace and Electronic Systems 51, no. 4 (2015): 2669–79. http://dx.doi.org/10.1109/taes.2015.130621.

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Asadabadi, Amirhossein, and Amir M. Anvar. "Small Satellite Modelling and Three-Axis Magnetorquer-Based Stabilisation Using Fuzzy Logic Control." Applied Mechanics and Materials 152-154 (January 2012): 1639–44. http://dx.doi.org/10.4028/www.scientific.net/amm.152-154.1639.

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Recently small satellites have become increasingly popular because of their ability to provide educational institutes with the chance to design, construct, and test their spacecraft from beginning to the possible launch due to the low launching cost and development of microelectronics (Figure 1). Clearly, using only electromagnetic coils instead of different types of actuators will serve the purpose of weight reduction where every grams counts. But some restrictions described in the paper limit utilising only “Electromagnetic” actuation for 3D stabilisation and adversely affects the efficiency
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Dissertations / Theses on the topic "Magnetorquer"

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Elmas, Tuba Cigdem. "Development Of Control Allocation Methods For Satellite Attitude Control." Master's thesis, METU, 2010. http://etd.lib.metu.edu.tr/upload/12611649/index.pdf.

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This thesis addresses the attitude control of satellites with similar and dissimilar actuators and control allocation methods on maneuvering. In addition, the control moment gyro (CMG) steering with gyroscopes having limited gimbal angle travel is also addressed. Full Momentum envelopes for a cluster of four CMG&#039<br>s are obtained in a pyramid type mounting arrangement. The envelopes when gimbal travel is limited to plus-minus 90 degree are also obtained. The steering simulations using Moore Penrose (MP) pseudo inverse as well as blended inverse are presented and success of the pre plann
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Bellini, Niccolo'. "Magnetic actuators for nanosatellite attitude control." Master's thesis, Alma Mater Studiorum - Università di Bologna, 2014. http://amslaurea.unibo.it/7506/.

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The research and the activities presented in the following thesis report have been led at the California Polytechnic State University (US) under the supervision of Prof. Jordi Puig Suari. The objective of the research has been the study of magnetic actuators for nanosatellite attitude control, called magnetorquer. Theese actuators are generally divided in three different kinds: air core torquer, embedded coil and torquerod. In a first phase of the activity, each technology has been analyzed, defining advantages and disadvantages, determining manufacturing procedures and creating mathematical
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Lehner, Maximilian Jacob. "Study and design of magnetic attitude control systems for nanosatellites." Bachelor's thesis, Alma Mater Studiorum - Università di Bologna, 2019.

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The objective of this bachelor thesis was to display all the attitude and control systems (ACS) available for CubeSats and how magnetic ACS are the most convenient option in terms of volume. Precisely this project focused on the procedure, the design and the laws of physics that are behind the creation of a torque rod, a magnetic attitude and control system conceived for nanosatellites. After discussing the magnetic laws, the different types of materials of the core, and the geometric parameters of the core and of the wire, all of which determine the operating area of the system, a theoretica
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Curatolo, Andrea. "Development and experimental testing of nanosatellites attitude control using mixed magnetic/mechanical actuation." Master's thesis, Alma Mater Studiorum - Università di Bologna, 2021. http://amslaurea.unibo.it/24337/.

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The Attitude Control System is one of the most important subsystems yet one of the least developed for what concerns the CubeSats. Magnetorquers are often employed as main actuators, thanks to their reduced dimensions. However, a spacecraft actuated by magnetorquers alone suffer from an instantaneous underactuation. Reaction wheels offer better performance but are prone to failure and must be desaturated periodically. It's possible to overcome the limits of both types of actuators by employing an ACS equipped with both types of actuators. In this work, an attitude control law integrating three
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Trégouët, Jean-François. "Synthèse de correcteurs robustes périodiques à mémoire et application au contrôle d'attitude de satellites par roues à réaction et magnéto-coupleurs." Thesis, Toulouse, ISAE, 2012. http://www.theses.fr/2012ESAE0033/document.

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Les travaux présentés dans ce mémoire constituent une contribution à la conception de méthodes systématiques pour l’analyse et la commande de systèmes périodiques et incertains. Une partie importante de cette thèse est également consacrée au contrôle d’attitude de satellites dont la dynamique se prête naturellement à une représentation sous forme de modèles périodiques soumis à des incertitudes. La première partie propose une présentation unifiée des résultats d’analyse et de synthèse de modèles périodiques et incertains à temps-discret via des méthodes basées sur des inégalités linéaires matr
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Greene, Michael R. "The Attitude Determination and Control System of the Generic Nanosatellite Bus." Thesis, 2009. http://hdl.handle.net/1807/18942.

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The Generic Nanosatellite Bus (GNB) is a spacecraft platform designed to accommodate the integration of diverse payloads in a common housing of supporting components. The development of the GNB at the Space Flight Laboratory (SFL) under the Canadian Advanced Nanospace eXperiment (CanX) program provides accelerated access to space while reducing non-recurring engineering (NRE) costs. The work presented herein details the development of the attitude determination and control subsystem (ADCS) of the GNB. Specific work on magnetorquer coil assembly, integration, and testing (AIT) and reaction whee
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Gondar, Rui Manuel Gomes. "Decentralized Control of Electromagnetic ChipSat Swarm Formations." Master's thesis, 2021. http://hdl.handle.net/10400.6/11700.

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Small satellite formation missions offer new options for space exploration and scientific experiments. Groups of satellites flying within short relative distances allow various important applications, such as spatially distributed instruments for atmospheric sampling or remote sensing systems. The ability to independently control the relative motion of each satellite is crucial to establish a swarm formation, using a large number of satellites moving along bounded relative trajectories. This type of mission poses several constraints on mass, size, and energy consumption; therefore, an au
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Book chapters on the topic "Magnetorquer"

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Eun, Youngho, Zihao Wang, and Xiaofeng Wu. "Parametric Study on the Magnetic Properties of the Electropermanent Magnetorquer." In Lecture Notes in Electrical Engineering. Springer Nature Singapore, 2022. http://dx.doi.org/10.1007/978-981-19-2635-8_21.

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Xiao, Wen, Xin Li, Ningning Zhang, Pengyu Zhang, Yinghui Gong, and Rongyan Ma. "A Distributive Control Method for Microsatellite Using the Biased Momentum Wheel and Magnetorquers." In Lecture Notes in Electrical Engineering. Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-15-8155-7_195.

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Bruni, Renato, and Fabio Celani. "Parameter Optimization for Spacecraft Attitude Stabilization Using Magnetorquers." In Advances in Spacecraft Attitude Control. IntechOpen, 2020. http://dx.doi.org/10.5772/intechopen.89197.

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Conference papers on the topic "Magnetorquer"

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Carabellese, Davide, Joshua S. Umansky-Castro, and Mason A. Peck. "Magnetorquer-only Nonlinear Attitude Control for CubeSats." In AIAA Scitech 2021 Forum. American Institute of Aeronautics and Astronautics, 2021. http://dx.doi.org/10.2514/6.2021-1099.

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Meili, Zhou, and Qi Hongyu. "Design of Three Axis Magnetorquer for Microsatellites." In 2013 Third International Conference on Instrumentation, Measurement, Computer, Communication and Control (IMCCC). IEEE, 2013. http://dx.doi.org/10.1109/imccc.2013.130.

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Eun, Youngho, Zihao Wang, and Xiaofeng Wu. "Performance Measure of the Novel Electropermanent Magnetorquer." In AIAA SCITECH 2023 Forum. American Institute of Aeronautics and Astronautics, 2023. http://dx.doi.org/10.2514/6.2023-0936.

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Torczynski, Daniel, Rouzbeh Amini, and Paolo Massioni. "Magnetorquer Based Attitude Control for a Nanosatellite Testplatform." In AIAA Infotech@Aerospace 2010. American Institute of Aeronautics and Astronautics, 2010. http://dx.doi.org/10.2514/6.2010-3511.

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Ali, Anwar, Leonardo Reyneri, Juan Carlos de los Rios, Haider Ali, and M. Rizwan Mughal. "Reconfigurable magnetorquer for the CubePMT module of CubeSat satellites." In 2012 15th International Multitopic Conference (INMIC). IEEE, 2012. http://dx.doi.org/10.1109/inmic.2012.6511478.

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"Small-satellite magnetorquer attitude control system modelling and simulation." In 20th International Congress on Modelling and Simulation (MODSIM2013). Modelling and Simulation Society of Australia and New Zealand (MSSANZ), Inc., 2013. http://dx.doi.org/10.36334/modsim.2013.c10.yi.

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Sokal, Ewelina, Roman Wawrzaszek, Grzegorz Juchnikowski, Jakub Adamiec, and Tomasz Zawistowski. "Design and test of magnetorquer in PCB technology for nanosatellites." In Photonics Applications in Astronomy, Communications, Industry, and High-Energy Physics Experiments 2019, edited by Ryszard S. Romaniuk and Maciej Linczuk. SPIE, 2019. http://dx.doi.org/10.1117/12.2537411.

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Eun, Youngho, Zhicheng Xie, Zihao Wang, and Xiaofeng Wu. "Operational Capabilities on the Nanosatellite Attitude Control Actuated by Electropermanent Magnetorquer." In 2022 22nd International Conference on Control, Automation and Systems (ICCAS). IEEE, 2022. http://dx.doi.org/10.23919/iccas55662.2022.10003682.

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Haryadi, Defrandi Renanda, Heroe Wijanto, Budi Syihabuddin, and Agus D. Prasetyo. "Design of attitude determination and control system using microstrip magnetorquer for nanosatellite." In 2016 International Conference on Control, Electronics, Renewable Energy and Communications (ICCEREC). IEEE, 2016. http://dx.doi.org/10.1109/iccerec.2016.7814974.

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Sugimura, Nobuo, Toshinori Kuwahara, and Kazuya Yoshida. "Attitude determination and control system for nadir pointing using magnetorquer and magnetometer." In 2016 IEEE Aerospace Conference. IEEE, 2016. http://dx.doi.org/10.1109/aero.2016.7500665.

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