Design, calibration and error analysis o
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Qin Xing; Jun Zhang; Min Qian; Zhenyuan Jia; Baoyuan Sun
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Article
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2011
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Elsevier Science
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English
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Small thrust liquid pulsed rocket engines operating in pulsed mode have gained a good reputation in attitude control applications for their potential reliability and efficiency. However, the pulsed characteristic creates a difficult measurement problem. In this paper, a novel thrust dynamometer with