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In-flight alignment of a strapdown inertial navigation system of an unmanned aerial vehicle. (English. Russian original) Zbl 1279.93081

J. Comput. Syst. Sci. Int. 52, No. 1, 106-116 (2013); translation from Izv. Ross. Akad. Nauk, Teor. Sist. Upravl. 2013, No. 1, 111-121 (2013).
Summary: The alignment system of a strapdown inertial navigation system for an unmanned aerial vehicle installed on a carrier aircraft is studied. The aim is to develop alignment techniques for the strapdown inertial navigation system that improve the accuracy of alignment and reduce the alignment time. A technique for constructing the initial alignment system for a strapdown inertial navigation system of an unmanned aerial vehicle is proposed.

MSC:

93C95 Application models in control theory
93A30 Mathematical modelling of systems (MSC2010)
70P05 Variable mass, rockets
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This reference list is based on information provided by the publisher or from digital mathematics libraries. Its items are heuristically matched to zbMATH identifiers and may contain data conversion errors. It attempts to reflect the references listed in the original paper as accurately as possible without claiming the completeness or perfect precision of the matching.