1974
DOI: 10.1002/j.2161-4296.1974.tb01199.x
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Mixed Inertial Navigation Systems For Surface Effect Ships

Abstract: High speed marine vehicles such as Surface Effect Ships impose several unique constraints on navigation system design. Particularly significant is the current lack of a reliable and accurate velocity sensor during high speed cruise operation. This paper describes the accuracy performance of several mixed inertial navigation systems which do not involve the use of a velocity sensor. Specifically considered are NAVSATINERTIAL, OMEGA‐INERTIAL, and NAVSAT‐OMEGA‐INERTIAL systems. The accuracy performance informatio… Show more

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Cited by 2 publications
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“…Inertial navigation produces an extremely precise measurement of aircraft position and attitude but has associated with it a reasonably large drift error in position which, if uncorrected, would prove to be unacceptable for many remote-sensing applications. This characteristic drift can be compensated for in hybrid systems in which data from a less precise but drift free sensor are also used [Beck, 1971;Sangiovanni and Moryl, 1974]. The system described here uses a visual sight to make periodic fixes on landmarks of known position to correct the drift error, resulting in track recovery accurate to + 10 m. This system has been investigated for use in flight path recovery for airborne survey operations [Grasty et al, 1977].…”
Section: Introductionmentioning
confidence: 99%
“…Inertial navigation produces an extremely precise measurement of aircraft position and attitude but has associated with it a reasonably large drift error in position which, if uncorrected, would prove to be unacceptable for many remote-sensing applications. This characteristic drift can be compensated for in hybrid systems in which data from a less precise but drift free sensor are also used [Beck, 1971;Sangiovanni and Moryl, 1974]. The system described here uses a visual sight to make periodic fixes on landmarks of known position to correct the drift error, resulting in track recovery accurate to + 10 m. This system has been investigated for use in flight path recovery for airborne survey operations [Grasty et al, 1977].…”
Section: Introductionmentioning
confidence: 99%