Data Mining pada Data Quick Access Recorder untuk Peningkatan Keselamatan Penerbangan
(1) Institut Teknologi Bandung
(2) Institut Teknologi Bandung
(*) Corresponding Author
Abstract
Keberadaan angin vertikal dan kekasaran permukaan landasan merupakanan parameter yang perlu diperhatikan terutama saat fase pendekatan (approach) hinggamendarat (landing)dan saat lepas landas (take-off) di bandar udara, karenakedua parameterdi atasmempengaruhi keselamatanpesawat udarasaat fase tersebut. Sementara itu,sampai saat ini belum ada peralatan yang dapat dipergunakan untuk melihat kecenderungan adanya angin vertikal maupun rendahnya koefisen gesek landasan. Makalah ini memaparkan teknik pengolahan data Quick Access Recorderuntuk mengestimasi parameter tersebut, kecepatan angin arah vertikal pada fase pendekatan sampai fase landingdan koefisien friksi runwaypada fase landing. Oleh karena kedua parameter di atas tidak direkam pada Quick Access Recorder maka diperlukan cara lain untuk mendapatkan parameter tersebut yaitu dengan teknik identifikasi sistem. Proses validasi dalam rangka meningkatkan keyakinan terhadap parameter yang diperoleh juga akan dilakukan. Teknik pengolahan data yang dipaparkan melibatkan dinamika gerak pesawat udara dan estimator. Bila semua airline memberikan data penerbangannya, tendensi keadanya angin vertikal dan penurunan koefisien friksi landasan akan segera didapatkan sehingga baik airline maupun bandar udara dapat melakukan antisipasi untuk keselamatan penerbangan.
[The Data Mining on Quick Access Recorder for Flight Safety Improvement] Vertical wind and runway surface roughness are the most concerned parameters when the aircraft initiating the procedures of approach-to-landing and take-off at an airport, due to they will affect the safety of the aircraft in those phases. In the meantime, there is no equipment that can be used to assess the chance of vertical wind emergence as well as the decline of runway surface friction. This paper describes Quick Access Recoder data processing technique for estimating those parameters, the speed of vertical wind in the approach-to-landing phase and runway friction coefficient in the landing phase. Due to those parameters does not recorded in Quick Access Recorder then system identification technique is utilized in order to obtain both of parameters. Validation process is sequenced to increase the confidence level. The described data processing technique involving the aircrafts motion dynamics and the estimator. In case all the airline provide their flight data, the tendency of vertical wind and the difference of runway friction can be calculated promptly so that the airline and the airport can take anticipation action for maintaining the safety level of the flight.
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Drees., Ludwig, Sembiring., Javensius, Holzapfel., Florian, et.al., IATA Safety Report 2013 Section 9 Predictive Analysis, April 2014
Sembiring., Javensius, Holzapfel., Florian, Extracting of Unmeasured Parameters Based on Quick Access Recorder Data Using Parameter Estimation Method, AIAA Atmospheric Flight Mechanics Conference, Boston, USA, Agustus 2013.
Sembiring., Javensius, Holzapfel., Florian, Bayesian Approach Implementation on Quick Access Recorder Data for Estimating Parameters and Model Validation, Probabilistic Safety Assessment and Management Conference, Hawaii, USA, Juni 2014.
DSouza., Christopher, Fundamendal of Kalman Filtering and Estimation in Aerospace Engineering, Bahan Kuliah Online, NASA, 2013.
Gelb., Arthur, Applied Optimal Estimation, The MIT Press, 2011.
Aldrich., John, R.A. Fisher and the Making of Maximum Likelihood 1912 -1922, Statistical Science, Institute of Mathematical Statistics, Agustus 1997.
https://en.wikipedia.org/wiki/Kalman_filter [Diakses pada 5 Mei 2016].
Jategaonkar., R.V., Flight Vehicle System Identification, A Time Domain Approach, AIAA Progress in Astronautics and Aeronautics, 2006
Klein., V., and Morelli., E., Aircraft System Identification: Theory and Practice, AIAA Progess in Astronautics and Aeronautics, 2006.
U.K Civil Aviation Authority, CAP 739 Flight Data Monitoring, 2013
Hongkong Civil Aviation Department, CAD 739 Flight Data Monitoring, A Guide to Implementation, Februari 2009.
Sembiring., Javensius, RTS Smoother Implementation on Quick Access Recorder Data, Presentasi video konferensi antara Flight Safety Research Group – Institute of Flight System Dynamics TUM dan AGS Sagem, Jerman, 1 Juni 2015
http://www.teledynecontrols.com/productsolution/airfase/overview.asp (Diakses pada 5 Mei 2016).
http://www.teledynecontrols.com/productsolution/wirelessgroundlink/groundlink.asp (Diakses pada 5 Mei 2016)
https://www.flightdataservices.com/ (Diakses pada 5 Mei 2016)
http://www.sagem.com/aerospace/commercial-aircraft/information-system/analysis-ground-station-ags (Diakses pada 5 Mei 2016)
http://www.aerobytes.co.uk/ (Diakses pada 5 Mei 2016)
ICAO, Annex 6 Part 1 Operation of Aircraft, Juli 2010
Menteri Perhubungan Republik Indonesia, Peraturan Menteri Perhubungan Nomor: PM 28 Tahun 2013 Tentang Peraturan Keselamatan Penerbangan Sipil Bagian 121, Maret 2013
EUROCAE, EUROCAE ED 112 Minimum Operational Performance Specification for Crash Protected Airborne Recorder Systems - Revision A, September 2013.
European Commision, Flightpath 2050 Europes Vision for Aviation, 2011
ICAO, DOC 9859 Safety Management Manual, Edisi 3, 2013
Boeing, Statistical Summary of Commercial Jet Airplane Accidents Worldwide Operation 1959; 2014, Agustus 2015
Airbus, Commerical Aviation Accidents 1958-2014-A Statistical Analysis, Mei 2014
DOI: http://dx.doi.org/10.25104/wa.v43i1.280.1-12
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