MFMC GBAS – Flight Trials and Performance Studies DLR.de Chart 1 ENC 2016 – Helsinki – 01.06.2016 M. Felux, M.-S. Circiu, D. Gerbeth

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Presentation transcript:

MFMC GBAS – Flight Trials and Performance Studies DLR.de Chart 1 ENC 2016 – Helsinki – M. Felux, M.-S. Circiu, D. Gerbeth

Protection against ionospheric gradient threat Ionospheric scintillation issues in high/low latitudes Weak constellations and required masking may have impact on performance Multi-Frequency Multi-Constellation GBAS Why? How? DLR.de Chart 2

Motivation Why? DLR.de Chart 3 Large ionospheric gradients and scintillation events can result in significant unavailability of the GBAS Graphic from: Hlubek N, Berdermann J, Wilken V, Gewies S, Jakowski N, et al.: Scintillations of the GPS, GLONASS, and Galileo signals at equatorial latitude. J. Space Weather Space Clim., 2014, 4, A22

Dual-frequency GBAS can tackle the ionospheric gradient problem Multi constellation GBAS can reduce the impact of scintillations on availability Quickly growing Galileo constellation (all satellites with E1/E5a) Currently 12 GPS Block IIF satellites with L1 and L5 operational, continuous launches all with second frequency Motivation How? DLR.de Chart 4

L5/E5a Satellite Status (12 GPS Block IIF, 14 (9) Galileo) DLR.de Chart 5 GPS Block IIF and Galileo status

Represented by protection levels: Need to determine all the necessary parameters for the processing modes Analysis of extesive ground and flight data to establish expectable performance models Performance Metric: Availability DLR.de Chart 6

Data Collection DLR.de Chart 7 Airbus A320 Dornier DO-228 Antenna: Antcom multiband Duration:100 hours A320 since May hours Dornier March 2015 Receiver: Javad Delta 23 Mhz bandwidth 2 correlator spacings

Towards MFMC GBAS – Performance Assessments Sigma air DLR.de Chart 8 Elevation in A/C body frame [deg]

DLR Ground Facility Braunschweig Airport L1L2L5 BR01 BR02 BR03 BR05 Javad Delta Receivers with GPS (L1/L2/L5) + Galileo (E1/E5a) + Glonass + BDS Connected to Leica AR25 choke ring antennas DLR.de Chart 9

Improved performance of the Galileo signals RX configuration: 0.1 chips correlator spacing (L1/E1) 1 chip correlator spacing (L5/E5a) Multipath and noise on Galileo E1 is lower than on GPS L1, especially at low elevation BOC(1,1) modulation Wider transmission bandwidth Galileo E5a shows lower multipath and noise than Galileo E1 BPSK(10) signal Higher chip rate Higher signal power Paper presented at ITM 2015 : M-S Circiu et. Al – “Evaluation of GPS L5, Galileo E1 and Galileo E5a Performance for Multi Frequency Multi Constellation GBAS” DLR.de Chart 10 Evaluating Performance of GPS L5 and Galileo E1/E5a Using Ground Measurements 10 GPS Block IIF, 4 Galileo 40 days of data – 100 sec smoothing constant

Dual-Frequency Dual-Constellation GBAS Flight Trials 4 flights in March 2015 with Dornier DO-228 (6h total) Satellite visibility: 5-7 dual frequency (GPS+Gal) Single-frequency L5/E5a GPS and GalileoDual-frequency L1/E1+L5/E5a GPS and Galileo DLR.de Chart 11

Protection Levels Contribution of Different Sigma Terms DLR.de Chart 12 GPS L1 30s (GAST D)GPS L5 30s

Protection Levels Contribution of Different Sigma Terms DLR.de Chart 13 GPS L1 30s (GAST D)GPS L1/L5 100s Ifree

‘Nominal Performance of Future Dual-Frequency Dual-Constellation GBAS’ In press, August 2016, IJAE Comparison and Trade-Off Studies 30s Smoothing Constant DLR.de Chart 14

‘Nominal Performance of Future Dual-Frequency Dual-Constellation GBAS’ In press, August 2016, IJAE Comparison and Trade-Off Studies 100s Smoothing Constant DLR.de Chart 15

Dual frequency and multi constellation GBAS can resolve many of the current GBAS issues More data and investigations needed for suitable models covering all aircraft, receivers, antennas etc. No solution to all problems No defined way ahead concerning different modes Trade-off is a difficult task Conclusions DLR.de Chart 16

Thank you for your attention! Questions? DLR.de Chart 17