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Original Articles

Design and development of a unit element microstrip antenna for aircraft collision avoidance system

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Pages 1732-1748 | Received 11 Jul 2016, Accepted 17 Apr 2017, Published online: 23 May 2017
 

ABSTRACT

Aircraft/traffic alert and collision avoidance system (ACAS/TCAS) is an airborne system which is designed to provide the service as a last defense equipment for avoiding mid-air collisions between the aircraft. In the existing system, four monopole stub-elements are used as ACAS directional antenna and one blade type element is used as ACAS omnidirectional antenna. The existing ACAS antenna has some drawbacks such as low gain, large beamwidth, frequency and beam tuning/scanning issues etc. Antenna issues like unwanted signals reception may create difficulties to identify the possible threats. In this paper, the focus is on the design and development of a unit element microstrip antenna which can be used for ACAS application and to overcome the possible limitations associated with the existing techniques. Two proposed antenna models are presented here, which are single feed and dual feed microstrip dual patch slotted antenna. These are designed and simulated in CST Microwave Studio tool. The performance and other antenna characteristics have been explored from the simulation results followed by the antenna fabrication and measurement. A good reflection coefficient, Voltage Standing Wave Ratio (VSWR), narrow beamwidth, perfect directional radiation pattern, high gain and directivity make this proposed antenna a good candidate for this application.

Acknowledgement

Authors would like to thank Space Application Centre (SAC), ISRO for proving the chance to explore their excellent measurement facilities during this research work. Authors are also very much glad to the college authority of National Institute of Technology, Rourkela, India, for various financial supports during this research work.

Disclosure statement

No potential conflict of interest was reported by the authors.

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