RENDEZVOUS AND DOCKING OF SPACECRAFT - ESA

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RGPS VERIFICATION SETUPSTIMULATOR SENSOR H/WGNC FUNCTIONCHASER POSITIONDISTUR−BANCESTARGETORBITALSTATEGPS SAT’SPOSITIONSTIMULATORTARGET GPS−RECEIVERH/WNAVIGATIONFILTERRV CONTROL SOFTWARE (CHASER)GUIDANCEFUNCTIONCONTROLFUNCTIONGPS SAT’SPOSITIONSTIMULATORDISTUR−BANCESCHASER GPS−RECEIVERH/WGYROS(MODEL)DISTUR−BANCESTARGET POSITIONCHASERORBITAL STATES/CDYNAMICS &KINEMATICSGPS−LAB FUNCTIONSRV SYSTEM SIMULATOR FUNCTIONSDr. W. Fehse — Introduction to RVD — Verification, Concepts & Tools — Version 2009110
STIMULATION FACILITY FOR OPTICAL SENSORS: EPOS(This figure shows the old EPOS facility with a gantry robot type of motion system)Gantry Robot 6 DOF, Target Mount 3 DOF, Illumination System 4 DOFDr. W. Fehse — Introduction to RVD — Verification, Concepts & Tools — Version 2009111
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RENDEZVOUS AND DOCKING OFSPACECRAFT
Page 3 and 4:
PART 1: INTRODUCTION TO RENDEZVOUS
Page 5 and 6:
THE SCENARIO IN LEOTHE LEO SCENARIO
Page 7 and 8:
THE INTERNATIONAL SPACE STATION (IS
Page 9 and 10:
SYSTEM AND FUNCTIONS IN GEO RVD (SC
Page 11 and 12:
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Page 13 and 14:
LAUNCH INTO THE ORBIT PLANE OF THE
Page 15 and 16:
DEFINITION OF PHASE ANGLEOrbital Pl
Page 17 and 18:
TRAJECTORIES IN EARTH CENTRED ANDTA
Page 19 and 20:
Hill EquationsFor circular orbits,
Page 21 and 22:
USE OFCLOHESSY-WILTSHIRE EQUATIONSA
Page 23 and 24:
IMPULSIVE TRAJECTORIESTANGENTIAL MA
Page 25 and 26:
THE PREDOMINANT DISTURBANCES IN LEO
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EFFECTS OF THE SOLAR PRESSURE IN GE
Page 29 and 30:
DRIVERS FOR RENDEZVOUS STRATEGIES I
Page 31 and 32:
DRIVERS FOR RVD STRATEGIES IN THE S
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COMMUNICATION RANGE OF GROUND STATI
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APPROACH STRATEGY EXAMPLE(JAPANESE
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Page 39 and 40:
THE PROBLEM OF CAPTURELAW OF CONSER
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Shock Attenuation DynamicsBasic Spa
Page 43 and 44:
TYPES OF DOCKING MECHANISMTWO BASIC
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Page 47 and 48:
THE AUTOMATIC ONBOARD CONTROL SYSTE
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CLOSED LOOP GNC BLOCK DIAGRAMSENSOR
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THE MISSION + VEHICLE MANAGEMENT (M
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FAULT TOLERANCE AND RECOVERY CONCEP
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COLLISION AVOIDANCE MANOEUVRE (CAM)
Page 57 and 58:
THE NAVIGATION REQUIREMENTS FOR ARD
Page 59 and 60: MEASUREMENT PRINCIPLES: RGPSRELATIV
Page 61 and 62: MEASUREMENT PRINCIPLE OF LASER RANG
Page 63 and 64: PART 1: INTRODUCTION TO RENDEZVOUS
Page 65 and 66: WHY DO WE WANT TO HAVE AN AUTOMATIC
Page 67 and 68: THE ROLE OF HUMAN OPERATORS INAUTOM
Page 69 and 70: THE TASKS OF GROUND OPERATORS IN AR
Page 71 and 72: RENDEZVOUS CONTROL SYSTEM DISPLAYPH
Page 73 and 74: WHAT IS DIFFERENT BETWEEN RVD IN GE
Page 75 and 76: THE MAJOR DIFFERENCES: ORBITAL DIST
Page 77 and 78: THE MAJOR DIFFERENCES:COMMUNICATION
Page 79 and 80: THE MAJOR DIFFERENCESGENERAL PROBLE
Page 81 and 82: ALLOCATION OF TASKS TO SPACE- AND G
Page 83 and 84: PART 2VERIFICATION & VALIDATION PRI
Page 85 and 86: GENERAL RVD VERIFICATION ISSUES (co
Page 87 and 88: DEFINITION OF VERIFICATION AND VALI
Page 91 and 92: VERIFICATION AND VALIDATIONIN THE D
Page 93 and 94: VERIFICATION IN THEFEASIBILITY STUD
Page 95 and 96: VERIFICATION IN THE EARLY DESIGN PH
Page 97 and 98: VERIFICATION IN THE FINAL DESIGN PH
Page 99 and 100: MERGING OF GNC, MVM AND FDIR IN O/B
Page 101 and 102: CLOSED LOOP GNC SIMULATION WITH O/B
Page 103 and 104: CLOSED LOOP GNC SIMULATION WITHREAL
Page 105 and 106: VERIFICATION IN THE FLIGHT ITEMMANU
Page 109: CLOSED LOOP GNC SIMULATION WITHREAL
Page 115 and 116: VERIFICATION OF CAPTURE IN THE DOCK
Page 117 and 118: VERIFICATION OF CAPTURE INTERFACESI
Page 121 and 122: CLOSED LOOP SIMULATION WITH O/B COM
Page 123 and 124: VALIDATION OF SIMULATION MODELS (co
Page 125: DEVELOPMENT LIFE CYCLE OF A SPACE P
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