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A Comprehensive Integrity Verification Architecture for On-Airport LAAS Category III Precision Landing
Comprehensive Integrity Architecture On-Airport LAAS Category III Precision Landing
2015/6/29
Future Local Area Augmentation System (LAAS)architectures will most likely be constrained to lie on airport property. Such a system must provide protection against rare events in the GPS Signal in Spa...
LAAS Sigma-Mean Monitor Analysis and Failure-Test Verification
LAAS Sigma-Mean Monitor Analysis Failure-Test Verification
2015/6/29
The Local Area Augmentation System (LAAS) is a ground-based differential GPS system being developed to support aircraft precision approach and landing navigation with guaranteed integrity. Stanford Un...
Verification of Low Latitude Ionosphere Effects on WAAS During October 2003 Geomagnetic Storm
Low Latitude Ionosphere Effects WAAS During Geomagnetic Storm
2015/6/26
The Federal Aviation Administration’s Wide Area Augmentation System (WAAS) provides high integrity GPS-based precision navigation service to users in the conterminous United States. In October 2003, o...
Prior Probability Model Development to Support System Safety Verification in the Presence of Anomalies
Prior Probability Model Development Support System Safety Verification
2015/6/26
Assessments of “prior probabilities” of faults that must be mitigated are essential to integrity and safety verification for safety-critical systems. In the case of Global Navigation Satellite System ...
Design and Hardware Verification of Canard Based Sounding Rocket Attitude Controller Using Adaptive Filter
Rockets Attitude Control Canard
2009/8/19
Canard based controller using an adaptive notch filter is proposed to control the attitude of launch vehicles including the ISAS's sounding rocket `S-520'. As the characteristics of launch vehicles ar...