Kalman Filtering Based Fault Tolerant Integrated INS/Radar Altimeter

Kalman Filtering Based Fault Tolerant Integrated INS/Radar Altimeter

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Navigation and guidance of a flight vehicle require that the altitude of the vehicle must be determined accurately. For this purpose different altimeter measurements can be integrated using Kalman filtering. In this monograph, the integrated navigation system, consisting of INS and radar altimeters, is presented. INS and the radar altimeter have different benefits and drawbacks. While having outstanding high frequency characteristics, the INS is a dead-reckoning system, at which the errors accumulate time by time. The radar altimeter, as a stand-alone system, gets timely updated measurements, ...