ΕΘΝΙΚΟ ΜΕΤΣΟΒΙΟ ΠΟΛΥΤΕΧΝΕΙΟ ΣΧΟΛΗ ΑΓΡΟΝΟΜΩΝ - ΤΟΠΟΓΡΑΦΩΝ ΜΗΧΑΝΙΚΩΝ ΚΕΝΤΡΟ ΔΟΡΥΦΟΡΩΝ ΔΙΟΝΥΣΟΥ

Σχετικά έγγραφα
APPENDIX B NETWORK ADJUSTMENT REPORTS JEFFERSON COUNTY, KENTUCKY JEFFERSON COUNTY, KENTUCKY JUNE 2016

4. Αεροτριγωνισμός Προετοιμασία Δεδομένων Επίλυση Αεροτριγωνισμού

Consolidated Drained

Συνόρθωση του δικτύου SmartNet Greece και ένταξη στο HTRS07 του HEPOS. Συγκρίσεις και εφαρμογές NRTK στην πράξη.

Ingenieurbüro Frank Blasek - Beratender Ingenieur Am Kohlhof 10, Osterholz-Scharmbeck Tel: 04791/ Fax: 04791/

Ingenieurbüro Frank Blasek - Beratender Ingenieur Am Kohlhof 10, Osterholz-Scharmbeck Tel: 04791/ Fax: 04791/

A Software Package Development for Estimating Atmospheric Path Delay based on Numerical Weather Prediction Model

ΤΕΧΝΙΚΗ ΕΚΘΕΣΗ 1. ΟΡΙΖΟΝΤΙΟΓΡΑΦΙΚΟ ΤΡΙΓΩΝΟΜΕΤΡΙΚΟ - ΥΨΟΜΕΤΡΙΚΟ ΔΙΚΤΥΟ.

Contents. 1 Introduction. 2 Shape of the Earth. 3 NAD 27 vs NAD 83

NMBTC.COM /

Project: 296 File: Title: CMC-E-600 ICD Doc No: Rev 2. Revision Date: 15 September 2010

HIS series. Signal Inductor Multilayer Ceramic Type FEATURE PART NUMBERING SYSTEM DIMENSIONS HIS R12 (1) (2) (3) (4)

Συνόρθωση και διαχρονικός έλεγχος του δικτύου METRICANET με μετρήσεις GNSS

Queensland University of Technology Transport Data Analysis and Modeling Methodologies

Ο ΗΓΙΕΣ ΧΡΗΣΗΣ GEKO 201

ΨΗΦΙΑΚΟ ΠΕ ΙΟΜΕΤΡΟ TRIMAX SM 2500

Rectangular Polar Parametric

TEXNIKH ΕΚΘΕΣΗ ΦΑΣΗ A - ΠΑΡΑΔΟΤΕΟ ΠΕ1 ( ) Συνόρθωση και διαχρονικός έλεγχος του δικτύου METRICANET με μετρήσεις GNSS

Reminders: linear functions

Artiste Picasso 9.1. Total Lumen Output: lm. Peak: cd 6862 K CRI: Lumen/Watt. Date: 4/27/2018

TRIAXIAL TEST, CORPS OF ENGINEERS FORMAT

Multilayer Chip Inductor


Characterization Report

ΕΓΧΕΙΡΙ ΙΟ ΧΡΗΣΗΣ ΠΡΟΓΡΑΜΜΑΤΟΣ

RSDW08 & RDDW08 series

Multilayer Ceramic Chip Capacitors

Photometric Data of Lamp

SECTION II: PROBABILITY MODELS

070-A

519.22(07.07) 78 : ( ) /.. ; c (07.07) , , 2008

ΜΕΘΟΔΟΙ ΥΠΟΛΟΓΙΣΜΟΥ ΤΗΣ ΖΕΝΙΘΕΙΑΣ ΤΡΟΠΟΣΦΑΙΡΙΚΗΣ ΥΣΤΕΡΗΣΗΣ ΣΕ ΜΟΝΙΜΟΥΣ ΣΤΑΘΜΟΥΣ GNSS

38 Te(OH) 6 2NH 4 H 2 PO 4 (NH 4 ) 2 HPO 4

NPIS Shielded Power Inductors

Table 1: Military Service: Models. Model 1 Model 2 Model 3 Model 4 Model 5 Model 6 Model 7 Model 8 Model 9 num unemployed mili mili num unemployed

CSR series. Thick Film Chip Resistor Current Sensing Type FEATURE PART NUMBERING SYSTEM ELECTRICAL CHARACTERISTICS

CORDIC Background (2A)

ΤΕΧΝΙΚΗ ΕΚΘΕΣΗ - ΠΑΡΑΔΟΤΕΟ ΠΕ1. Διαχρονική επίλυση του δικτύου METRICANET GNSS και ποιοτικός έλεγχος

Multilayer Ceramic Chip Capacitors

AT Surface Mount Package SOT-363 (SC-70) I I Y. Pin Connections B 1 C 1 E 1 E 2 C 2 B , 7:56 PM

Approximation of distance between locations on earth given by latitude and longitude

DETERMINATION OF DYNAMIC CHARACTERISTICS OF A 2DOF SYSTEM. by Zoran VARGA, Ms.C.E.

IV. ANHANG 179. Anhang 178

Aluminum Electrolytic Capacitors

for fracture orientation and fracture density on physical model data

SMD Transient Voltage Suppressors

Numerical Methods for Civil Engineers. Lecture 10 Ordinary Differential Equations. Ordinary Differential Equations. d x dx.

Λογαριθμικά Γραμμικά Μοντέλα Poisson Παλινδρόμηση Παράδειγμα στο SPSS

Aluminum Electrolytic Capacitors (Large Can Type)

Summary of the model specified

Technical Information T-9100 SI. Suva. refrigerants. Thermodynamic Properties of. Suva Refrigerant [R-410A (50/50)]

SPECIFICATIONS. PRODUCT NAME: AC COB15W LED module (3120) General Customer MODEL NAME: CUSTOMER P/N: DATE:

Appendix A3. Table A3.1. General linear model results for RMSE under the unconditional model. Source DF SS Mean Square

Technical Report. General Design Data of a Three Phase Induction Machine 90kW Squirrel Cage Rotor

! " # $ &,-" " (.* & -" " ( /* 0 (1 1* 0 - (* 0 #! - (#* 2 3( 4* 2 (* 2 5!! 3 ( * (7 4* 2 #8 (# * 9 : (* 9


Τέτοιες λειτουργίες γίνονται διαμέσου του

Cycloaddition of Homochiral Dihydroimidazoles: A 1,3-Dipolar Cycloaddition Route to Optically Active Pyrrolo[1,2-a]imidazoles

SURTEC TEST REPORT. 9, Kon Jan North Road Liutu Industrial Zone Keelung,# 206, Taiwan RDT B

4 Way Reversing Valve

EVERFINE GONIOPHOTOMETERS SYSTEM TEST REPORT Page 1 Of 9

Homework 8 Model Solution Section

Electronic Supplementary Information (ESI)

Metal Oxide Varistors (MOV) Data Sheet

Numerical simulation of Earth s gravitational field recovery from SST based on the energy conservation principle

DuPont Suva 95 Refrigerant

3o/B Mάθημα: Δικτύωμα / 2D-Truss in Batch

FORMULAS FOR STATISTICS 1

Surface Mount Multilayer Chip Capacitors for Commodity Solutions

Digital motor protection relays

Data sheet Thick Film Chip Resistor 5% - RS Series 0201/0402/0603/0805/1206

The Global Positioning System

DuPont Suva 95 Refrigerant

DESIGN OF MACHINERY SOLUTION MANUAL h in h 4 0.

Supplementary Materials for Evolutionary Multiobjective Optimization Based Multimodal Optimization: Fitness Landscape Approximation and Peak Detection

Main source: "Discrete-time systems and computer control" by Α. ΣΚΟΔΡΑΣ ΨΗΦΙΑΚΟΣ ΕΛΕΓΧΟΣ ΔΙΑΛΕΞΗ 4 ΔΙΑΦΑΝΕΙΑ 1

Statistics 104: Quantitative Methods for Economics Formula and Theorem Review

FEATURES APPLICATION PRODUCT T IDENTIFICATION PRODUCT T DIMENSION MAG.LAYERS

Monolithic Crystal Filters (M.C.F.)

Εργαστήριο Ανάπτυξης Εφαρμογών Βάσεων Δεδομένων. Εξάμηνο 7 ο

Eισαγωγή στο λογισμικό QGis

Aquinas College. Edexcel Mathematical formulae and statistics tables DO NOT WRITE ON THIS BOOKLET

Project: Brimsmore, Ye... Job no: C08127 Designed By kristian Checked By Network W Network Design Table for OUTFALL B.SWS

Αξιολόγηση του ΕΓΣΑ87 μέσω ενός σύγχρονου γεωδαιτικού μοντέλου ταχυτήτων για τον Ελλαδικό χώρο

DuPont Suva. DuPont. Thermodynamic Properties of. Refrigerant (R-410A) Technical Information. refrigerants T-410A ENG

DATA SHEET Surface mount NTC thermistors. BCcomponents

Does anemia contribute to end-organ dysfunction in ICU patients Statistical Analysis

Α ρ ι σ τ ο τ έ λ ε ι ο Π α ν ε π ι σ τ ή μ ι ο Θ ε σ σ α λ ο ν ί κ η ς Μ Ε Τ Α Π Τ Υ Χ Ι Α Κ Η Ε Ρ Γ Α Σ Ι Α

συναρτησιακό μοντέλο: Ax=l+v (γεωμετρική απόσταση δορυφόρων-δέκτη) μετρήσεις: l στοχαστικό μοντέλο: W=σ 02 V (ψευδοαποστάσεις) (σ i =c cosecφ i )

Surface Mount Aluminum Electrolytic Capacitors

High Performance Voltage Controlled Amplifiers Typical and Guaranteed Specifications 50 Ω System

S

SAW FILTER - RF RF SAW FILTER

SMD Power Inductor. - SPRH127 Series. Marking. 1 Marking Outline: 1 Appearance and dimensions (mm)

OWA-60E series IP67. 60W Single Output Moistureproof Adaptor. moistureproof. File Name:OWA-60E-SPEC

CORDIC Background (4A)

ΕΙΣΑΓΩΓΗ ΣΤΗ ΣΤΑΤΙΣΤΙΚΗ ΑΝΑΛΥΣΗ

Wan Nor Arifin under the Creative Commons Attribution-ShareAlike 4.0 International License. 1 Introduction 1

Finish: Anticorrosive finish in polyester. Number of motor poles 4=1400 r/min. 50 Hz 6=900 r/min. 50 Hz 8=750 r/min. 50 Hz

PROPERTIES OF ORDINARY WATER SUBSTANCE AT SATURATION FROF TME CRITICAL POINT DOWN TO 66 C EQUATIONS & TABLES

Transcript:

GPSEST ----------- TABLE OF CONTENTS -- 1. CAMPAIGNS 2. OBSERVATION FILES 3. GENERAL OPTIONS 4. STATIONS 5. SATELLITE ORBITS 6. ATMOSPHERE 7. RECEIVER CLOCK PARAMETERS 8. POLE COORDINATES AND TIME INFORMATION 9. ANTENNA PHASE CENTERS 10. CONSTANTS 11. PARAMETER CHARACTERIZATION LIST 12. TEST OUTPUT 13. RESULTS (PART 1) 14. RESULTS (PART 2) -----------

------------ -------------- LIST OF INPUT AND OUTPUT FILENAMES ----------- GENERAL CONSTANTS : X:\GEN\CONST. SINEX GENERAL INPUT FILE : X:\GEN\SINEX. IONEX CONTROL FILE : X:\GEN\IONEX. POLE INFORMATION : X:\GEN\JMK2.ERP LOCAL GEODETIC DATUM : X:\GEN\DATUM. SATELLITE INFO : X:\GEN\SATELLIT.TTT SATELLITE PROBLEMS : X:\GEN\SAT_2002.CRX PHASE CENTER ECCENTRICITIES : X:\GEN\PHAS_IGS.01B APRIORI COORDINATES : C:\JMK\STA\ITRF96.CRD STANDARD ORBITS : C:\JMK\ORB\112.STD RADIATION PRESSURE COEFF. : --- IONOSPHERE MODELS : --- CODE BIAS INPUT FILE : --- ANTENNA ORIENTATIONS : --- TROPOSPHERE ESTIMATES INPUT : --- SITE ECCENTRICITIES : --- OCEAN LOADING TABLES : --- SATELLITE CLOCKS : --- ANTENNA ORIENTATIONS : --- COORDINATE RESULTS : C:\JMK\STA\GGRS.CRD ORBIT RESULTS : --- IONOSPHERE RESULTS : --- CODE BIAS OUTPUT FILE : --- ANTENNA RESULTS (GRID) : --- ANTENNA RESULTS (HARM) : --- IONEX OUTPUT FILE : --- VAR/COVAR MATRIX COORD. : --- VAR/COVAR MATRIX TOTAL : --- NORMAL EQUATIONS : --- RESIDUALS : --- EARTH ROTATION PARAMETERS : --- IERS FORMAT ERP OUTPUT : ---

TROPOSPHERE CORRECTIONS : --- TROPOSPHERE GRADIENTS : --- TROPOS. SINEX OUTPUT : --- GRID PHASE CENTER OUTPUT : --- HARM. PHASE CENTER OUTPUT : --- SATELLITE CLK. FILE : --- ----------- ----------- 1. CAMPAIGNS ------------ CAMPAIGN NAME NUM STATION NAME NUM STATION NAME NUM STATION NAME NUM STATION NAME NUM STATION NAME ----------- JMK : 7 227020 3 JMK-T1-2000 2. OBSERVATION FILES ----- ----------- JMK

----------- MAIN CHARACTERISTICS: ----- FILE OBSERVATION FILE HEADER OBSERVATION FILE SESS ----------- 1 C:\JMK\OBS\TRT11120.PSH C:\JMK\OBS\TRT11120.PSO 1120 AMB.I.+S. #CLUSTERS FILE TYP FREQ. STATION 1 STATION 2 SESS FIRST OBSERV.TIME #EPO DT #EF #CLK ARC #SAT W 12 #AMB L1 L2 L5 RM ----------- 1 P L1 227020 JMK-T1-2000 1120 2-04-22 13:33:00 446 15 0 E E 1 7 N Y N 7 1 1 7 0 SATELLITES: ---------- FILE #SAT SATELLITES ----------- 1 7 1 3 11 14 20 21 25 OBSERVATION SELECTION: ------ SAMPLING RATE : 0 SEC ELEVATION CUT-OFF ANGLE : 15 DEGREES

----------- 3. GENERAL OPTIONS --- A PRIORI SIGMA OF UNIT WEIGHT: -------------- A PRIORI SIGMA OF UNIT WEIGHT : 0.002 M (SIGMA OF ONE-WAY L1 PHASE OBSERVABLE AT ZENITH) MODEL FOR ELEVATION-DEPENDENT WEIGHTING : 1/COS(Z) CORRELATIONS AND SESSIONS: ---------- STRATEGY : CORRELATIONS CORRECTLY MODELLED TIME INTERVAL : 1.00000 SEC (TO IDENTIFY EPOCH) SESS #FILE FILE NUMBERS ----------- 1120 1 1 AMBIGUITY RESOLUTION STRATEGY: -------------- AMBIGUITIES PRE-ELIMINATED ONCE PER SESSION

SYNCHRONIZATION ERRORS: ------- STRATEGY : SYNCHRONIZATION ERRORS NOT APPLIED ----------- 4. STATIONS ----------- LOCAL GEODETIC DATUM: ----- DATUM NAME ELL. PARAM./ SCALE SHIFTS TO WGS-84 ROTATIONS TO WGS-84 ----------- ITRF96 A = 6378137.000 M DX = 0.0000 M RX = 0.00000 " 1/F= 298.2572221 DY = 0.0000 M RY = 0.00000 " SC = 0.00000D+00 DZ = 0.0000 M RZ = 0.00000 " A PRIORI STATION COORDINATES: C:\JMK\STA\ITRF96.CRD ------------- WGS-84 COORDINATES IN METERS ELLIPSOIDAL COORDINATES IN LOCAL DATUM NUM STATION NAME OBS E/F/C X Y Z LATITUDE LONGITUDE HEIGHT (M)

----------- 7 227020 Y FIXED 4581562.5510 2168945.8880 3858504.6450 37 27 49.481754 25 19 59.605504 219.7093 3 JMK-T1-2000 Y ESTIM 4582873.1827 2170838.1250 3855824.9555 37 26 1.144457 25 20 46.360562 173.6554 27-MAY-02 10:34 SOFTWARE VERSION 4.2 ---------- - 5. SATELLITE ORBITS ---- ARC CHARACTERISTICS: ---- ARC START OF ARC END OF ARC SOURCE #SAT SATELLITES ---------- - 22 1 02-04-22 0:00:00 02-04-23 0:00:00 PR2002.112 27 1 2 3 4 5 6 7 8 9 10 11 13 14 15 18 20 21 23 24 25 26 27 28 29 30 31 OSCULATING ELEMENTS: ---- C:\JMK\ORB\112.STD REFERENCE SYSTEM: J2000.0 REFERENCE EPOCH : 52386.5645833 MJD (2002 4 22 13 33 0.00)

SAT S.MAJ.AXIS ECCENTRIC. INCLINAT. NODE PERIGEE M. ANOMALY PER.PASS.TIME ----------- 1 26559141.1 0.00529675 55.495010 84.076613-96.853243 35.111923 52386.5159571 2 26558504.1 0.02202284 53.450746-161.913465-112.119062-18.975708 52386.5908617 3 26562304.4 0.00313145 53.480647-100.202090-327.693086 148.944786 52386.3582741 4 26561499.5 0.00588184 55.586290-35.650320-17.523724-5.145961 52386.5717109 5 26562803.3 0.00366740 53.631910-160.657167 30.942786-22.167164 52386.5952888 6 26559998.3 0.00645908 53.908991-97.485234-127.591108 45.759140 52386.5012088 7 26559904.5 0.01197121 54.010279-99.175907-112.393546 161.346565 52386.3411262 8 26562137.0 0.00816203 54.994125 144.680231 122.973665 54.248701 52386.4894421 9 26559094.8 0.01290392 54.204346 141.414996 46.417322 25.815306 52386.5288320 10 26560944.3 0.00504617 56.180718 23.137651 6.853060-136.809416 52386.7540688 11 26559191.6 0.00053475 52.579026-40.706614-59.111313 130.995352 52386.3831685 13 26557552.2 0.00201940 55.736766 82.915006 7.840694-95.332108 52386.6965961 14 26561158.9 0.00218282 55.430168 82.615066-37.405625 79.591018 52386.4543458 15 26561492.2 0.00841314 55.967159-32.949174-254.287699 81.150088 52386.4521843 18 26560860.7 0.00257345 55.204955 25.677584 169.202610-29.514976 52386.6054623 20 26561509.8 0.00199528 55.239372 22.695787 106.813593-104.661090 52386.7095470 21 26558480.8 0.01811231 56.162488 23.472461 225.751256-115.155029 52386.7240546 22 26559574.3 0.01516007 53.420964-161.135251 44.621196-153.385456 52386.7770108 23 26559963.2 0.01591238 56.358597 25.935247-100.464809-73.346072 52386.6661644 24 26559801.4 0.00915854 56.165078-34.568050-89.866881 32.260442 52386.5199045 25 26561027.5 0.00982343 53.795493 138.872955-106.073909 76.015044 52386.4592995 26 26560499.1 0.01361325 55.657704 83.166366 19.285067 133.117548 52386.3802158 27 26560875.0 0.01613048 54.055369 140.287518-140.047241-10.331289 52386.5788924 28 26559316.1 0.00629050 54.979763-157.007906 218.712292-102.033979 52386.7058907 29 26540401.6 0.00841637 55.480409 81.437337 253.649152-140.260746 52386.7586237 30 26563148.5 0.00619345 54.037639-158.600000 75.915970-92.504217 52386.6927206 31 26562166.4 0.01093908 53.979411-99.196119 51.733210 94.670555 52386.4334525 SATELLITE PROBLEMS: --- SAT PROBLEM TYPE ACTION FROM TO

----------- 12 BAD PHASE+CODE OBS. REMOVED 97-06-04 0:00:00 99-12-31 23:59:59 16 BAD PHASE+CODE OBS. REMOVED 00-09-14 0:00:00 99-12-31 23:59:59 32 BAD PHASE+CODE OBS. REMOVED 90-01-01 0:00:00 99-12-31 23:59:59 102 BAD PHASE+CODE OBS. REMOVED 00-01-01 0:00:00 99-12-31 23:59:59 110 BAD PHASE+CODE OBS. REMOVED 99-09-05 0:00:00 99-12-31 23:59:59 114 BAD PHASE+CODE OBS. REMOVED 99-07-08 0:00:00 99-12-31 23:59:59 115 BAD PHASE+CODE OBS. REMOVED 01-01-29 0:00:00 99-03-31 23:59:59 101 BAD PHASE+CODE OBS. REMOVED 00-01-01 0:00:00 99-12-31 23:59:59 108 BAD PHASE+CODE OBS. REMOVED 00-01-01 0:00:00 99-12-31 23:59:59 117 BAD PHASE+CODE OBS. REMOVED 00-01-01 0:00:00 99-12-31 23:59:59 118 BAD PHASE+CODE OBS. REMOVED 00-01-01 0:00:00 99-12-31 23:59:59 124 BAD PHASE+CODE OBS. REMOVED 00-01-01 0:00:00 99-12-31 23:59:59 ----------- 6. ATMOSPHERE ------------- TROPOSPHERE MODEL: -- NO TROPOSPHERE CORRECTIONS APPLIED SITE-SPECIFIC TROPOSPHERE PARAMETERS: ------ MAPPING FUNCTION USED FOR DELAY ESTIMATION: DRY NIELL

TROPOSPHERE GRADIENT ESTIMATION : NO PAR STATION NAME VALIDITY START VALIDITY END SIG_N (M) SIG_E (M) SIG_U (M) ABS/REL ----------- 1 227020 2002 04 21 24.0 2002 04 22 6.0 5.00000 ABS 2 227020 2002 04 22 6.0 2002 04 22 12.0 5.00000 REL 3 227020 2002 04 22 12.0 2002 04 22 18.0 5.00000 REL 4 227020 2002 04 22 18.0 2002 04 23 0.0 5.00000 REL 5 JMK-T1-2000 2002 04 21 24.0 2002 04 22 6.0 5.00000 ABS 6 JMK-T1-2000 2002 04 22 6.0 2002 04 22 12.0 5.00000 REL 7 JMK-T1-2000 2002 04 22 12.0 2002 04 22 18.0 5.00000 REL 8 JMK-T1-2000 2002 04 22 18.0 2002 04 23 0.0 5.00000 REL IONOSPHERE MODELS: -- NO IONOSPHERE MODELS APPLIED ----------- 8. POLE COORDINATES AND TIME INFORMATION ---------- A PRIORI POLE AND TIME INFORMATION FORM THE POLE FILE: -------- DATUM TIME X-POLE (") Y-POLE (") UT1-UTC (S) GPS-UTC (S) RMS XP (") RMS YP (") RMS DT (S) EP-CPO (") PS-CPO (") RMS EP (") RMS PS (")

----------- 02-04-22 12:00:00 0.03630 0.55510-0.201859 13. 0.00003 0.00003 0.000009 0.00000 0.00000 0.00000 0.00000 02-04-23 12:00:00 0.03949 0.55492-0.202780 13. 0.00003 0.00003 0.000010 0.00000 0.00000 0.00000 0.00000 CELESTIAL POLE OFFSET MODEL: NO MODEL SUBDAILY POLE MODEL: RAY ----------- 11. TEST OUTPUT MIN. AND MAX. ELEVATION ANGLES AND MAX. SYNCHRONIZATION ERRORS: -- SESS FILE STATION NAME 1 STATION NAME 2 MIN/MAX ELEV. SYNCH. ERR. (NS) ----------- 1120 1 227020 JMK-T1-2000 15.0 83.7 0.0

----------- 12. RESULTS (PART 1) ----- NUMBER OF PARAMETERS (PART 1): -------------- PARAMETER TYPE #PARAMETERS #PRE-ELIMINATED #SET-UP #NO-OBS #REF #SINGULAR ----------- STATION COORDINATES 3 0 3 0 0 0 AMBIGUITIES 0 0 (BEFORE INV) 1 1 0 0 SITE-SPECIFIC TROPOSPHERE PARAMETERS 8 0 8 0 0 0 ----------- TOTAL NUMBER OF PARAMETERS 11 0 12 1 0 0 ----------- NUMBER OF OBSERVATIONS (PART 1): - TYPE FREQUENCY FILE #OBSERVATIONS ----------- PHASE L1 ALL 1727

----------- TOTAL NUMBER OF OBSERVATIONS 1727 ----------- A POSTERIORI SIGMA OF UNIT WEIGHT (PART 1): ------------ A POSTERIORI SIGMA OF UNIT WEIGHT : 0.0028 M (SIGMA OF ONE-WAY L1 PHASE OBSERVABLE AT ZENITH) DEGREE OF FREEDOM (DOF) : 1716 CHI**2/DOF : 2.00 ----------- STATION COORDINATES: C:\JMK\STA\GGRS.CRD ---- NUM STATION NAME PARAMETER A PRIORI VALUE NEW VALUE NEW- A PRIORI RMS ERROR 3-D ELLIPSOID 2-D ELLIPSE ----------- 3 JMK-T1-2000 X 4582873.1827 4582872.9644-0.2183 0.0020 Y 2170838.1250 2170837.3504-0.7746 0.0011 Z 3855824.9555 3855824.7012-0.2543 0.0015

0.0003 77.6 HEIGHT 173.6554 173.0809-0.5746 0.0025 0.0025 7.2 LATITUDE 37 26 1.144457 37 26 1.148334 0.1197 0.0009 0.0003 77.9 LONGITUDE 25 20 46.360562 25 20 46.335887-0.6051 0.0003 0.0009-0.3 0.0009 ----------- SITE-SPECIFIC TROPOSPHERE PARAMETERS: (NOT SAVED) ------ CORRECTIONS (M) RMS ERRORS (M) ZENITH VECTOR (") ERROR ELLIPSE (M) REQU. STATION NAME NORTH EAST ZENITH NORTH EAST ZENITH ANGLE RMS RATIO AZI MAX RMS MIN RMS AZI ----------- 1 227020-0.84476 5.47614 2 227020-1.68952 4.47295 3 227020-4.22381 0.33782 4 227020-2.11190 5.00148 5 JMK-T1-2000 -0.84580 5.47614 6 JMK-T1-2000 -1.69160 4.47295 7 JMK-T1-2000 -4.22899 0.33820 8 JMK-T1-2000 -2.11449 5.00149

GPS ----------- RMS ERRORS OF ELLIPS. COORDINATES AND COORDINATE DIFFER. IN MM (PART 1): ------------- ----- NUM 3 ----- B 0.9 3 L 0.3 H 2.5 ----- ----------- SLOPE DISTANCES AND RMS ERRORS IN M (PART 1): ---------- NUM 7 F ---------- 3 O 3532.5702 N N 3532.2673 RMS 0.0009 ----------