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IS-GNSS 2014 Jeju, South Korea Oct. 22, 2014 MSAS Status Takeyasu Sakai Electronic Navigation Research Institute, Japan Takeyasu Sakai Electronic Navigation.

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Presentation on theme: "IS-GNSS 2014 Jeju, South Korea Oct. 22, 2014 MSAS Status Takeyasu Sakai Electronic Navigation Research Institute, Japan Takeyasu Sakai Electronic Navigation."— Presentation transcript:

1 IS-GNSS 2014 Jeju, South Korea Oct. 22, 2014 MSAS Status Takeyasu Sakai Electronic Navigation Research Institute, Japan Takeyasu Sakai Electronic Navigation Research Institute, Japan

2 IS-GNSS Oct. 2014 - Slide 1 Contents Current Status MSAS User Segment & PBN LPV Approach Trial R&D for Performance Improvement

3 IS-GNSS Oct. 2014 - Slide 2 Current Status   MSAS: Japanese SBAS in operation. – –MTSAT Satellite-based Augmentation System. – –Operational since Sept. 27, 2007. Test signal since summer 2005. – –Continue stable operation with 2 GEOs.   Service for Air Navigation – –GPS Augmentation Information for RNAV, from En-route through NPA (RNP 0.3).   Within Fukuoka FIR.   Horizontal navigation only due to ionosphere. – –NOTAM is available to MSAS users.   Alert for Service Interruption.   Alert for Predicted Service Outage.

4 IS-GNSS Oct. 2014 - Slide 3 Configuration 2 GEO, 2 MCS (Master Control Station), 4 GMS (Ground Monitor Station), and 2 MRS;2 GEO, 2 MCS (Master Control Station), 4 GMS (Ground Monitor Station), and 2 MRS; MCS also has GMS function; MSAS has 6 domestic monitor stations.MCS also has GMS function; MSAS has 6 domestic monitor stations. 2 MRS (Monitor and Ranging Station) for GEO positioning for GEO ranging function.2 MRS (Monitor and Ranging Station) for GEO positioning for GEO ranging function. 6 GMS in Japan CanberraMRS HawaiiMRS MSAS Monitor Stations

5 IS-GNSS Oct. 2014 - Slide 4 MSAS GEO (MTSAT) 3-axis stabilized spacecraft with the standard bus system.3-axis stabilized spacecraft with the standard bus system. Solar panel at the single side.Solar panel at the single side. –Due to installation of equipment for the weather mission. L-band transponder with the bandwidth of 2.2MHz.L-band transponder with the bandwidth of 2.2MHz. –Uplink: Ku-band (13GHz) due to results of frequency coordination. Also has downlink channel in Ku-band.Also has downlink channel in Ku-band. –For power control of uplink signal because of rain attenuation in Ku-band. MTSAT-1R Spacecraft

6 IS-GNSS Oct. 2014 - Slide 5 MCS Facilities KASC (Kobe Aeronautical Satellite Center) HASC (Hitachi-Ota Aeronautical Satellite Center) Western part of JapanWestern part of Japan MCS nominal for MTSAT-1R (PRN129)MCS nominal for MTSAT-1R (PRN129) Backup for MTSAT-2 (PRN137)Backup for MTSAT-2 (PRN137) Dishes for 2 GEO and emergencyDishes for 2 GEO and emergency Eastern part of JapanEastern part of Japan MCS nominal for MTSAT-2 (PRN137)MCS nominal for MTSAT-2 (PRN137) Backup for MTSAT-1R (PRN129)Backup for MTSAT-1R (PRN129) Dishes for 2 GEODishes for 2 GEO

7 IS-GNSS Oct. 2014 - Slide 6 MTSAT Coverage (Fukuoka FIR) FIR: Flight Information Region MTSAT-1R @140E MTSAT-2 @145E

8 IS-GNSS Oct. 2014 - Slide 7 Performance of MSAS GEONET 940058 (Takayama) 08/1/17-19 PRN129 (MTSAT-1R) Broadcast Signal GPS only w/ MSAS Horizontal 0.425m RMS E-W N-S GPS only w/ MSAS Vertical 0.607m RMS E-W U-D

9 IS-GNSS Oct. 2014 - Slide 8 Integrity Performance From 2013/7/17 To 2013/8/16 (1 month) (1 month) MSAS PRN137 Evaluated at: HASC GME-A HASC GME-A HAL=556m Loss of Availability Normal Operation Loss of Availability & Integrity Loss of Integrity Loss of Integrity Actual Error, m Horizontal Protection Level (HPL), m Enroute to NPAEnroute to NPA Extremely safe operationExtremely safe operation

10 IS-GNSS Oct. 2014 - Slide 9 MSAS Users in Aviation Regional Air carriers Fire Fighters Medical Government

11 IS-GNSS Oct. 2014 - Slide 10 New Japanese Aircraft w/SBAS Mitsubishi Regional Jet (MRJ) – –70-90 seat Schedule: Now Assembly Work. – –First flight is scheduled for 3Q 2015. – –First delivery of MRJ is slated for 3Q 2017. Rockwell Collins ‘Pro Line Fusion’ has a LPV capability. Purchase Agreement with ANA 25 aircraft, JAL 32 aircraft, Trans States Holdings 100 aircraft, and SkyWest 200 aircraft. Mitsubishi Regional Jet MRJ

12 IS-GNSS Oct. 2014 - Slide 11 Implementation of RNP/RNAV

13 IS-GNSS Oct. 2014 - Slide 12 LPV Approach Trial Gulfstream-IV JA001G / JA002G SAAB 2000 JA003G / JA004G Bombardier BD-700 JA005G / JA006G Bombardier DHC-8-300 JA007G Flight Inspection Aircraft of JCAB Upgraded FMS to support SBAS LPV approach

14 IS-GNSS Oct. 2014 - Slide 13 DHC-8 Upgraded for LPV EADI Announciator EHSI MLS= MSAS Landing System? (They used I/F for MLS, micro-wave landing system)

15 IS-GNSS Oct. 2014 - Slide 14 Trial at Fukushima AP LPV Approach Chart for Test Flight ( Fukushima Airport ) On 16 July, 2010 Test Flight at Fukushima On 16 July, 2010 Test Flight at Fukushima LPV Announciator ON Start Approach Captain Side: LPV Co-Pilot Side: ILS Start Approach Captain Side: LPV Co-Pilot Side: ILS EADI/EHSI indicate same as ILS Indicate ‘0.0NM’ over the runway threshold HPL: 17.4m < HAL: 40m VPL: 31.3m < VAL: 50m GPS: 11 SV Completed LPV Approach with MSAS !! Database for LPV App = ILS Overlay at Fukushima, Niigata, Kouchi, Miho.

16 IS-GNSS Oct. 2014 - Slide 15 Performance Improvement Provide Vertical Guidance – –APV-I (LPV) or hopefully CAT-I (LPV200) performance. Hardware and Software Upgrade – –Addition of up to 10 Ground Monitor Stations. – –Installation of new algorithm developed by the ENRI. The current system uses the algorithm same as IOC WAAS. The algorithm should be improved to adapt to the Japanese ionosphere conditions which are more severe than U.S. and mitigate ionosphere effect. Motivation

17 IS-GNSS Oct. 2014 - Slide 16 Performance Improvement Current MSASEnhanced MSAS 08/1/17 APV-I Availability 6 GMS Planar Fit 08/1/17 LPV-200 Availability 16 GMS + New Ionospheric Algorithm The simulation result showing possibilities to improve the performance of MSAS.

18 IS-GNSS Oct. 2014 - Slide 17 Near-Term Outlook: Current Plan FY 05 FY 06 FY 07 FY 08 FY 09 FY 10 FY 11 FY 12 FY 13FY14 FY 15 FY 16 FY 17 FY 18 FY 19 FY 20 FY 21 MTSAT-1R Operation MTSAT-2 Operation 4-year life extension Single satellite operation term MSAS Commission Decision Making Year Future Satellite Systems EoL of MTSAT-1R is forecasted as the end of 2014. Expect the extension of EoL of MTSAT-2 for 4 years. After EoL of MTSAT-1R, MSAS will be operated with 1 GEO. – –Both KASC and HASC will operate with MTSAT-2. Discussion on a successor to MSAS is ongoing: Other GEO project…

19 IS-GNSS Oct. 2014 - Slide 18 Conclusion MSAS has been operational since Sept. 2007.MSAS has been operational since Sept. 2007. –An operational SBAS in accordance with ICAO standards. –Stable operation with two GEOs and two MCSs. –Continue to serve with Enroute to NPA performance. MSAS GEO:MSAS GEO: –Currently operating with MTSAT-1R/MTSAT-2 GEOs. –End of life of the 2 nd GEO is extended, but in 2020. –Currently discussing the plan beyond 2020. Contact: sakai@enri.go.jpContact: sakai@enri.go.jp


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