作者: F. Sansone , F. Branz , A. Francesconi , M. Barbetta , M. G. Pelizzo
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摘要: This paper presents the 2D close-range navigation sensor for cooperative spacecraft developed in framework of experiment ARCADE. The exploits an infrared LED transmitter mounted on target, and two photodiode receivers chaser. Laboratory tests were performed to assess performance range application. accuracies estimates were, average, 1.9 mm distance 1.0 deg yaw angle, ranges [0.20, 0.42] m [-40, 40] deg, respectively.