Hybrid fault detection and isolation techniques for aircraft inertial measurement sensors

Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference

Volumn 5, Issue , 2004, Pages 3399-3417

  Kim, Seungkeun ^a,b   Kim, Youdan ^a,b   Park, ChanGook ^a,b   Jung, Insung ^a,c  

^a Seoul National University   (South Korea)

^b Department of Aerospace Engineering ^*  (South Korea)

^c LG Electronics Inc   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT INERTIAL MEASUREMENT SENSORS; HYBRID FAULT DETECTION; ISOLATION TECHNIQUES; UNMANNED AERIAL VEHICLES (UAV);

COMPUTER SIMULATION; INERTIAL NAVIGATION SYSTEMS; KALMAN FILTERING; MATHEMATICAL MODELS; ROBUSTNESS (CONTROL SYSTEMS); SENSORS; UNMANNED VEHICLES;

AIRCRAFT MODELS;

EID: 19944363856     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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