Title :
Integration of local area augmentation system and inertial navigation system for aircraft surface movement guidance
Author_Institution :
Ohio Univ., Athens, OH, USA
Abstract :
The research presented is aimed at developing a positioning system that can support aircraft surface movement guidance for commercial aircraft in all weather conditions while maintaining traffic flow equivalent to visual meteorological conditions. Runway incursion trends suggest that the safety margin during the surface operation is reducing. An advanced surface movement guidance system for all surface vehicles operating on airport property could significantly diminish this trend. The proposed system is designed to provide high accuracy position information to an aircraft from touchdown through rollout, turnoff and taxi to the gate area and vice-versa from pushback to takeoff position
Keywords :
Kalman filters; air traffic control; aircraft landing guidance; collision avoidance; ground support systems; inertial navigation; aircraft surface movement guidance; all-weather conditions; commercial aircraft; complementary Kalman filter; ground facility; high accuracy position information; inertial navigation system; integrated system; local area augmentation system; positioning system; runway incursion; safety margin; Air traffic control; Aircraft navigation; Airports; Antenna arrays; Dipole antennas; Inertial navigation; Instruments; Meteorology; Position measurement; Traffic control;
Conference_Titel :
Digital Avionics Systems Conference, 2000. Proceedings. DASC. The 19th
Conference_Location :
Philadelphia, PA
Print_ISBN :
0-7803-6395-7
DOI :
10.1109/DASC.2000.886916