DocumentCode :
2910987
Title :
Mid- air collision prevention in aircraft using GLARE algorithm
Author :
Pais, Larwin Arnold ; Prakash, A. J Arun Jeya ; Sharma, Gaurav
Author_Institution :
Dept. of Aeronaut. Eng., Hindustan Univ., Chennai, India
fYear :
2011
fDate :
5-12 March 2011
Firstpage :
1
Lastpage :
4
Abstract :
(TCAS) Traffic collision avoidance system) is a technique used to reduce mid -air collision. It was developed by the Federal aviation administration (FAA), civil aviation authorities (CAA) and the aviation industry. However past analysis shows that there are late reactions or human errors such as over reactions from pilot´s which may lead to flight crash or injuries to passengers. There may also be a lack of communication between (ATC) and crew when a resolution advisories (RA) occurs. In this paper, we propose a autopilot configured TCAS that would help to reduce mid air collisions. This can be done using a MSP-430(DSP Microcontroller) that takes coordinates from transponders, and judge any critical scenario based on the GLARE algorithm and shift to autopilot mode until the aircraft reaches a safe zone. Whenever a (TA) occurs the control shifts to longitudinal autopilot mode until the aircraft reaches a safe position; then shifts back to pilot mode. This prevents the pilot from taking control whenever a TA occurs, thus preventing human effort.
Keywords :
air traffic control; aircraft control; collision avoidance; microcontrollers; DSP microcontroller; Federal aviation administration; GLARE algorithm; MSP-430; air traffic control; aircraft; autopilot configured TCAS; aviation industry; civil aviation authorities; longitudinal autopilot mode; mid-air collision prevention; resolution advisories; traffic collision avoidance system; Air traffic control; Aircraft; Elevators; Humans; Microcontrollers; Servomotors; Transponders;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2011 IEEE
Conference_Location :
Big Sky, MT
ISSN :
1095-323X
Print_ISBN :
978-1-4244-7350-2
Type :
conf
DOI :
10.1109/AERO.2011.5747527
Filename :
5747527
Link To Document :
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