{"status":"ok","message-type":"work","message-version":"1.0.0","message":{"indexed":{"date-parts":[[2024,7,28]],"date-time":"2024-07-28T16:30:40Z","timestamp":1722184240031},"reference-count":16,"publisher":"Emerald","issue":"2","license":[{"start":{"date-parts":[[2018,6,11]],"date-time":"2018-06-11T00:00:00Z","timestamp":1528675200000},"content-version":"tdm","delay-in-days":0,"URL":"https:\/\/www.emerald.com\/insight\/site-policies"}],"content-domain":{"domain":[],"crossmark-restriction":false},"short-container-title":["IJICC"],"published-print":{"date-parts":[[2018,6,11]]},"abstract":"\nPurpose<\/jats:title>\nThe three-axis simulator relies on the air film between the air bearing and the bearing seat to achieve weightlessness and the frictionless motion condition, which is essential for simulating the micro-disturbance torque of a satellite in outer space. However, at the beginning of the experiment, the disturbance torque caused by the misalignment between the center of gravity of the simulator and the center of rotation of the bearing is the most important factor restricting the use of the space three-axis simulator. In order to solve this problem, it is necessary to set the balance adjustment system on the simulator to compensate the disturbance torque caused by the eccentricity. The paper aims to discuss these issues.<\/jats:p>\n<\/jats:sec>\n\nDesign\/methodology\/approach<\/jats:title>\nIn this paper, a study of L1 adaptive automatic balancing control method for micro satellite with motor without other actuators is proposed. L1 adaptive control algorithm adds the low-pass filter to the control law, which in a certain sense to reduce the high-frequency signal and speed up the response time of the controlled system. At the same time, by estimating the adaptive parameter uncertainty in object, the output error of the state predictor and the controlled object can be stabilized under Lyapunov condition, and the robustness of the system is also improved. The automatic balancing method of PID is also studied in this paper.<\/jats:p>\n<\/jats:sec>\n\nFindings<\/jats:title>\nThrough this automatic balancing mechanism, the gravity disturbance torque can be effectively reduced down to 10\u22126<\/jats:sup>\u2009Nm, and the automatic balancing time can be controlled within 7\u2009s.<\/jats:p>\n<\/jats:sec>\n\nOriginality\/value<\/jats:title>\nThis paper introduces an automatic balancing mechanism. The experimental results show that the mechanism can greatly improve the convergence speed while guaranteeing the control accuracy, and ensuring the feasibility of the large angle maneuver of spacecraft three-axis simulator.<\/jats:p>\n<\/jats:sec>","DOI":"10.1108\/ijicc-07-2017-0084","type":"journal-article","created":{"date-parts":[[2018,4,23]],"date-time":"2018-04-23T23:13:07Z","timestamp":1524525187000},"page":"269-284","source":"Crossref","is-referenced-by-count":3,"title":["A study of PID and L1 adaptive control for automatic balancing of a spacecraft three-axis simulator"],"prefix":"10.1108","volume":"11","author":[{"given":"Bing","family":"Hua","sequence":"first","affiliation":[]},{"given":"Lin","family":"Chen","sequence":"additional","affiliation":[]},{"given":"Yunhua","family":"Wu","sequence":"additional","affiliation":[]},{"given":"Zhiming","family":"Chen","sequence":"additional","affiliation":[]}],"member":"140","reference":[{"key":"key2020092813201169300_ref001","volume-title":"Research on Technical Implementation of Three-Axis Air Bearing System","year":"2012"},{"issue":"1","key":"key2020092813201169300_ref002","doi-asserted-by":"crossref","first-page":"197","DOI":"10.2514\/1.60380","article-title":"Automatic mass balancing of a spacecraft three-axis simulator: analysis and experimentation","volume":"37","year":"2014","journal-title":"Journal of Guidance, Control, and Dynamics"},{"key":"key2020092813201169300_ref003","volume-title":"Automatic Mass Balancing System for the 5-DOF Spacecraft Simulator","year":"2016"},{"key":"key2020092813201169300_ref004","first-page":"94464P","article-title":"Parameter estimation of an air-bearing suspended test table","year":"2015","journal-title":"International Symposium on Precision Engineering Measurement and Instrumentation. International Society for Optics and Photonics, Vol. 9446"},{"issue":"10","key":"key2020092813201169300_ref005","first-page":"1224","article-title":"Design for the Six-DOF air bearing table and automatic mass balancing system of attitude platform","volume":"27","year":"2016","journal-title":"Journal of Astronautics"},{"issue":"1","key":"key2020092813201169300_ref006","first-page":"77","article-title":"From PID to L1 adaptive control for automatic balancing of a spacecraft three-axis simulator","volume":"6","year":"2016","journal-title":"Exploring Research and Innovations"},{"key":"key2020092813201169300_ref007","first-page":"21","article-title":"System identification and automatic mass balancing of ground-based three-axis spacecraft simulator","year":"2006"},{"issue":"3","key":"key2020092813201169300_ref008","doi-asserted-by":"crossref","first-page":"1005","DOI":"10.2514\/1.34437","article-title":"Automatic mass balancing of air-bearing based three-axis rotational spacecraft simulator","volume":"32","year":"2009","journal-title":"Journal of Guidance, Control, and Dynamics"},{"key":"key2020092813201169300_ref009","first-page":"1420","article-title":"An air bearing table for satellite attitude control simulation","year":"2015"},{"key":"key2020092813201169300_ref010","volume-title":"L1 Adaptive Control for Hypersonic Vehicle in Near Space","year":"2012"},{"issue":"12","key":"key2020092813201169300_ref011","first-page":"1265","article-title":"An improved L1 control for attitude regulation","volume":"35","year":"2015","journal-title":"Transactions of Beijing Institute of Technology"},{"issue":"5","key":"key2020092813201169300_ref012","first-page":"1124","article-title":"Automatic mass balancing of three-axis rotational spacecraft simulator","volume":"37","year":"2015","journal-title":"Systems Engineering and Electronics"},{"key":"key2020092813201169300_ref013","doi-asserted-by":"crossref","first-page":"254","DOI":"10.1016\/j.actaastro.2015.08.010","article-title":"Parameter estimation of a three-axis spacecraft simulator using recursive least-squares approach with tracking differentiator and extended Kalman filter","volume":"117","year":"2015","journal-title":"Acta Astronautica"},{"key":"key2020092813201169300_ref014","first-page":"1","article-title":"Automatic mass balancing of a spacecraft simulator based on non-orthogonal structure","year":"2016"},{"key":"key2020092813201169300_ref015","volume-title":"Research on a Method for Automatic Mass Balancing of Air-Bearing Based Three-Axis Rotational Satellite Simulator","year":"2014"},{"key":"key2020092813201169300_ref016","volume-title":"Research on Balance System on the Three Axis Air Bearing Platform","year":"2009"}],"container-title":["International Journal of Intelligent Computing and Cybernetics"],"original-title":[],"language":"en","link":[{"URL":"https:\/\/www.emerald.com\/insight\/content\/doi\/10.1108\/IJICC-07-2017-0084\/full\/xml","content-type":"application\/xml","content-version":"vor","intended-application":"text-mining"},{"URL":"https:\/\/www.emerald.com\/insight\/content\/doi\/10.1108\/IJICC-07-2017-0084\/full\/html","content-type":"unspecified","content-version":"vor","intended-application":"similarity-checking"}],"deposited":{"date-parts":[[2020,9,28]],"date-time":"2020-09-28T13:20:26Z","timestamp":1601299226000},"score":1,"resource":{"primary":{"URL":"https:\/\/www.emerald.com\/insight\/content\/doi\/10.1108\/IJICC-07-2017-0084\/full\/html"}},"subtitle":[],"short-title":[],"issued":{"date-parts":[[2018,6,11]]},"references-count":16,"journal-issue":{"issue":"2","published-print":{"date-parts":[[2018,6,11]]}},"alternative-id":["10.1108\/IJICC-07-2017-0084"],"URL":"https:\/\/doi.org\/10.1108\/ijicc-07-2017-0084","relation":{},"ISSN":["1756-378X"],"issn-type":[{"value":"1756-378X","type":"print"}],"subject":[],"published":{"date-parts":[[2018,6,11]]}}}