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Inertial Navigation Systems: Prelaunch Alignment
IRE Transactions on Aeronautical and Navigational Electronics, 1962A conventional inertial navigation system navigates by sensing components of the acceleration vector along three mutually perpendicular axes held stable after some initial alignment. This paper discusses the need for initial alignment, followed by a review of the effects of alignment errors on navigation in order to establish the order of accuracies ...
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Inertial Sensors and Navigation Systems
2015Highly precise and reliable indigenous inertial sensors and navigation systems, developed ab initio, have contributed immensely to the success of space launch vehicles of India. The venue of development was the erstwhile space science and technology center, since outgrown into, Vikram Sarabhai Space Centre, VSSC, Indian Space Research Organization ...
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