METHODS AND INSTRUMENTS FOR NONCONTACT DIAGNOSTICS OF THE TCAS SYSTEM

Islam Asad Isgandarov, Seymur MirMustafa Karimov, Nergiz Huseyn Babayeva

Abstract


This article is devoted to an investigation of the TCAS (Traffic Collision Avoidance System) diagnostics and self-diagnostics problems. The aim of the current research is to prepare the TCAS system built-in diagnostics aid and to build a model of a device for non-contact monitoring of the TCAS unit operational status. The tasks of the research are the following: to conduct analysis of the features and capabilities of the TCAS diagnostic techniques and aids; to develop a model which can detect the spurious actuation of the system and false decision-making; to prepare techniques which can detect such behavior of the system during a flight; to construct a model of a device for built-in diagnostics based on an non-contact monitoring of the TCAS states. The applied techniques of the researches are the following: application of signs, facts, and heuristic information about faults, implementation of an instrumental approach and diagnostic techniques based on an estimation of measured and monitored parameters. The system state monitoring method was proposed to carry out non-contact diagnostics of the system and to monitor the operating modes. This method is based on operating current variations by means of current measure using non-contact meters. It was proposed to apply the Hall sensor and the Rogowski coil to carry out such diagnostics. The schematic model to monitor the operation of the TCAS receiving and computing unit is developed considering Hall sensors’ capabilities to measure both direct and alternating currents. It was proposed the method and schematics to monitor TCAS system transmitter operating modes due to the fact that Rogowski coil is capable to measure both pulse and HF currents. This promotes to carry out diagnostics of the system proper operation. Several model versions of Rogowski coil are developed. Researches were carried out applying self-contained testing device (АКИП – 3407/2А) and Tektronics TSB digital oscilloscope. Conclusions. The novelty of the carried researches is follows: it is proposed a method for monitoring the variations of operating currents applied by the TCAS basic units for providing the self-contained diagnostics system; it is proposed a method for monitoring the system state according to the operating current variations, based on current measurements applying the Hall sensor and the Rogowski coil to provide the TCAS non-contact diagnostics. The research includes analysis of the laboratory measurements which were performed applying several versions of the Rogowski coil. Functional diagrams of the coil connections to the circuit are developed applying MultiSim14. The logical unit of the TCAS electrical modes built-in monitoring device is developed applying MatLab and MultiSim14


Keywords


TCAS; false decisions; operating current; non-contact diagnostics; Hall sensor; Rogowski coil

Full Text:

PDF

References


Pashayev, A. M., Iskenderov, I. A., Huseynov, V. S. Peculiarities of the electrical systems of flight equipments and problems of control to their operating parameters. Bulletin of the Azerbaijan Engineering Academy, B., 2014, vol. 6, no. 1, p. 59-66.

Boeing-767. Training manual. BK-767FSL-301R0-NAV-2OF2-98191. 441 p.

Cary R. Spitzer. The Avionics Handbook. AvioniCon, Inc. Williamsburg, Virginia, 2011. 541 p.

Cessna Aircraft Company. CAS-67A Traffic Alert and Collision Avoidance System (TCAS II). ICA Supplement. Model No: 525A. Supplement No: ICA-525A-34-00003. Supplement date: 6/15/2015. 44 p.

Chen, Dehuang. Wang, Xiaowei., Zhao, Jing. Aircraft Maintenance Decision System Based on Real-time Condition Monitoring. The First Aeronautical College of Air Force Xinyang 464000, China Lingyun GroupWuhan 430040, China, Procedia Engineering 29, 2012, pp. 765 – 769.

Honeywell. Hall effect sensing and application. Micro switch sensing and control, printed in USA. 126 p.

Honeywell. System Installation Manual. CAS 67A. TCAS II System. Manual Number 006-05340-0007. Revision 7 September 2004. 484 p.

Iskenderov, I. A., Babayeva, N. H. The model of autonomous diagnostic of TCAS system from situation of the false work and incorrect decision-making. Journal of Scientists Notes, NAA, Baku, 2018, vol. 20, no. 2.

Iskenderov, I. A. To the application of modern voltage and current sensors in the aircraft's onboard equipment. Journal of Scientists Notes, NAA, Baku, 2016, vol. 18, no. 4.

Kuchar, James K., Drumm, Ann C. The Traffic Alert and Collision Avoidance System. Lincoln laboratory journal, 2007, vol. 16, no. 2, pp. 277-296.

Koelle, Joshua., Smith, Matthew., Sulcs, Peter., Kacprzynski, Greg. and Walthall, Rhonda. Lessons Learned in Implementing a Practical Aircraft System Health Management (ASHM) System. Impact Technologies, a Sikorsky Innovations Company, Rochester, NY, 14623, USA. UTC Aerospace Systems, San Diego, CA, 92123, USA. 8 p.

Przytula, K. Wojtek., Allen, David., Vian, John., Mansouri, Gary. Health monitoring for commercial aircraft systems. HRL Laboratories, LLC, Malibu, CA 90265. The Boeing Company, Phantom Works, Seattle, WA 98124. 26TH International Congress of the Aeronautical Sciences. 8 p.

Paun, Maria-Alexandra., Sallese, Jean-Michel and Kayal, Maher. Hall Effect Sensors Design, Integration and Behavior Analysis. Journal of Sensor and Actuator Networks, ISSN 2224-2708, 8 February 2013, pp. 85-97.

Samimi, Mohammad Hamed., Mahari, Arash., Farahnakian, Mohammad Ali., Mohseni, Hossein. A Review on the Rogowski Coil Principles and Applications. IEEE Sensors Journal, October 2014. 8 p.




DOI: https://doi.org/10.32620/aktt.2018.6.11