RENDEZVOUS AND DOCKING OF SPACECRAFT - ESA

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©©©©©©©©©©©©¡ ¢ ¢ ¡ §§§ ¨¨¨¨ ¨¨§§§ ¦¥¥¥¥¥ ¦ ¦ ¦ ¦¥¤¦¤¥¥¥££££££££ ¤ ¤ ¤ ¤ ¤£¤£££TYPES OF DOCKING MECHANISM (DIAGRAM)CENTRAL DOCKING MECHANISMPERIPHERAL DOCKING MECHANISMPETALS CAN BE INSIDEOR OUTSIDEAT HATCH OPENING, MECHANISM IS IN THE WAYIN CASE OF CENTRAL DOCKING MECHANISMDr. W. Fehse – Introduction to RVD – Capture Issues – Version 200944
PART 1: INTRODUCTION TO RENDEZVOUS & DOCKINGTHE MOST IMPORTANT QUESTIONS TO BEANSWERED1. WHAT ARE THE TASKS, WHAT IS THE SCENARIO, WHO ARE THEMAJOR PLAYERS IN A RENDEZVOUS MISSION ?2. HOW DOES THE APPROACHING VEHICLE GET FROM GROUNDTO THE TARGET ?3. WHAT ARE THE MAIN ISSUES OF CAPTURE IN SPACE ?4. WHICH FUNCTIONS MUST BE AVAILABLE ABOARD TO DO ITAUTOMATICALLY (LEO) ?5. WHAT IS THE ROLE OF MAN IN THE AUTOMATIC RENDEZVOUSPROCESS (LEO)?6. WHAT ARE THE MAIN ISSUES OF RENDEZVOUS & CAPTURE IN GEO ?Dr. W. Fehse – Introduction to RVD – Automatic RVD Onboard Functions – Version 200945
Page 1 and 2: 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: ¨©¡¡¡¡ ¢¢£££¢¢¢£££
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
Page 27 and 28: 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
Page 33 and 34: COMMUNICATION RANGE OF GROUND STATI
Page 35 and 36: APPROACH STRATEGY EXAMPLE(JAPANESE
Page 39 and 40: THE PROBLEM OF CAPTURELAW OF CONSER
Page 41 and 42: Shock Attenuation DynamicsBasic Spa
Page 43: TYPES OF DOCKING MECHANISMTWO BASIC
Page 47 and 48: THE AUTOMATIC ONBOARD CONTROL SYSTE
Page 49 and 50: CLOSED LOOP GNC BLOCK DIAGRAMSENSOR
Page 51 and 52: THE MISSION + VEHICLE MANAGEMENT (M
Page 53 and 54: FAULT TOLERANCE AND RECOVERY CONCEP
Page 55 and 56: 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 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 89 and 90: PART 2VERIFICATION & VALIDATION PRI
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 107 and 108:
PART 2VERIFICATION & VALIDATION PRI
Page 109 and 110:
CLOSED LOOP GNC SIMULATION WITHREAL
Page 111 and 112:
STIMULATION FACILITY FOR OPTICAL SE
Page 113 and 114:
Page 115 and 116:
VERIFICATION OF CAPTURE IN THE DOCK
Page 117 and 118:
VERIFICATION OF CAPTURE INTERFACESI
Page 119 and 120:
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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RENDEZVOUS AND DOCKING OF SPACECRAFT - ESA

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