Guidance and Control Conference 1977
DOI: 10.2514/6.1977-1109
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Redundant integrated flight control/navigation inertial sensor complex

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“…Furthermore, these aircraft generally require two inertial units, one for the control of the vehicle and the other for navigation data. It is only recently that fighter aircraft such as the Eurofighter have implemented a single inertial unit for the dual purpose of control and navigation (Ebner and Mark 1978). In all cases, however, the sensors employed, and in particular the gyros, are of high performance.…”
Section: Configuration Of Redundant Inertial Sensorsmentioning
confidence: 99%
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“…Furthermore, these aircraft generally require two inertial units, one for the control of the vehicle and the other for navigation data. It is only recently that fighter aircraft such as the Eurofighter have implemented a single inertial unit for the dual purpose of control and navigation (Ebner and Mark 1978). In all cases, however, the sensors employed, and in particular the gyros, are of high performance.…”
Section: Configuration Of Redundant Inertial Sensorsmentioning
confidence: 99%
“…The method is simple and popular. However, parity space methods have problems with singularities caused by the relationship between the configuration of the sensors and the motion of the vehicle (Ebner and Mark 1978). Faults cannot be detected within these singularities.…”
Section: Inertial Navigationmentioning
confidence: 99%