发明名称 SYSTEMS AND METHODS FOR ATTITUDE FAULT DETECTION BASED ON INTEGRATED GNSS/INERTIAL HYBRID FILTER RESIDUALS
摘要 Systems and methods for attitude fault detection based on integrated GNSS/inertial hybrid filter residuals are provided. In one embodiment, a fault detection system for aircraft attitude measurement system comprises: a sensor monitor coupled to a first inertial measurement unit, the sensor monitor comprising: a navigation error model for the first inertial measurement unit, the model configured to model a plurality of error states including at least an attitude error state vector, an velocity error state vector, and a position error state vector determined from data generated by the first inertial measurement unit; and a propagator-estimator configured to propagate and update error states based on GNSS data; and a residual evaluator configured to input measurement error residual values generated by the propagator-estimator, wherein the residual evaluator outputs an alert signal when the measurement error residual values exceed a threshold.
申请公布号 US2016290826(A1) 申请公布日期 2016.10.06
申请号 US201414564359 申请日期 2014.12.09
申请人 Honeywell International Inc. 发明人 Brenner Mats Anders;Ahlbrecht Mark A.;Morrison John R.
分类号 G01C23/00;G07C5/08;G05D1/08;B64D47/00 主分类号 G01C23/00
代理机构 代理人
主权项 1. A fault detection system for aircraft attitude measurement system, the fault detection system comprising: a sensor monitor coupled to a first inertial measurement unit of the aircraft attitude measurement system, the sensor monitor comprising: a navigation error model for the first inertial measurement unit, the navigation error model configured to model a plurality of error states including at least an attitude error state vector, an velocity error state vector, and a position error state vector determined from data generated by the first inertial measurement unit; anda propagator-estimator configured to propagate and update the plurality of error states from the navigation error model based on GNSS data; and a residual evaluator configured to input measurement error residual values generated by the propagator-estimator, wherein the residual evaluator outputs an alert signal when the measurement error residual values exceed a predetermined statistical threshold.
地址 Morristown NJ US