Accuracy Improvement by Boundary Conditions for Inertial Navigation
نویسندگان
چکیده
منابع مشابه
Improvement of Navigation Accuracy using Tightly Coupled Kalman Filter
In this paper, a mechanism is designed for integration of inertial navigation system information (INS) and global positioning system information (GPS). In this type of system a series of mathematical and filtering algorithms with Tightly Coupled techniques with several objectives such as application of integrated navigation algorithms, precise calculation of flying object position, speed and at...
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ژورنال
عنوان ژورنال: International Journal of Navigation and Observation
سال: 2010
ISSN: 1687-5990,1687-6008
DOI: 10.1155/2010/869127