Precision Navigation Achieved by ASTRO-H Space-borne GPS Receiver
نویسندگان
چکیده
منابع مشابه
Computationally Efficient Unscented Kalman Filtering Techniques for Launch Vehicle Navigation using a Space-borne GPS Receiver
The Extended Kalman Filter (EKF) is a well established technique for position and velocity estimation. However, the performance of the EKF degrades considerably in highly non-linear system applications as it requires local linearisation in its prediction stage. The Unscented Kalman Filter (UKF) was developed to address the non-linearity in the system by deterministic sampling. The UKF provides ...
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a DIIAR c/o Polo of Como, Politecnico of Milan, Piazza Leonardo Da Vinci 32, 20133 Milano, Italy [email protected] b DIMeC, University of Modena and Reggio Emilia, via Vignolese 905/B, 41100 Modena, Italy (marco.dubbini, capra.alessandro, cristina.castagnetti)@unimore.it c Department of Mathematics, University of Modena and Reggio Emilia, Via Campi 213/B, 41100 Modena, Italy francesco.un...
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ژورنال
عنوان ژورنال: TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
سال: 2018
ISSN: 1884-0485
DOI: 10.2322/tastj.16.454