- Page 8: viiiLIST OF FIGURESFigurePage1.1 Si
- Page 11 and 12: 2consisting of all objects in Earth
- Page 13 and 14: 4Figure 1.3 Monthly Number of Objec
- Page 15 and 16: 6Figure 1.4 Debris Cloud History Af
- Page 17 and 18: 8will serve both military and civil
- Page 19 and 20: 10continue, but those developments
- Page 21 and 22: 12The use of sweeper devices to rem
- Page 23 and 24: 14Figure 1.9 Collision Probabilitie
- Page 25 and 26: 16Figure 1.10 Orbit Lifetime Guidel
- Page 27 and 28: 181.3.2 Terminal Rendezvous between
- Page 29 and 30: 20Figure 1.13 ETS-VII Experiment.Th
- Page 32: 23propulsion systems covered a rang
- Page 35 and 36: 261.4 Description of the GlobalStar
- Page 37 and 38: 28Figure 1.17 GlobalStar Spacecraft
- Page 39 and 40: 30CHAPTER 2IMPULSIVE ORBIT TRANSFER
- Page 41 and 42: 32⃗ ̇ ⃗ ⃗ ⃗ (2.4)and the a
- Page 43 and 44: 34Figure 2.3 Position Vector of Cha
- Page 45 and 46: 36⃗⃗⃗⃗ ∆ ⃗ (2.14)Substi
- Page 47 and 48: 38Figure 2.4 Co-moving Clohessy-Wil
- Page 49 and 50: 40Combining equations Equations (2.
- Page 51 and 52: 42∆ ̇ ∆ ̇ [ ( )∆ ∆ ̇ ( )
- Page 53 and 54:
44Observe that we have dropped the
- Page 55 and 56:
46* + [ ⃗⃗ ( )]*∆ ⃗ + [ ⃗
- Page 57 and 58:
48CHAPTER 3DEVELOPMENT OF ∆V BUDG
- Page 59 and 60:
50nodes (RAAN or Ω)—five satelli
- Page 61 and 62:
25164U25872U25885U25964U25771U25874
- Page 63 and 64:
54aerodynamic drag, third-body pert
- Page 65 and 66:
56GlobalStar satellite target orbit
- Page 67 and 68:
58GS-25964U - MSCO2 8167.01 km 6.98
- Page 69 and 70:
60Figure 3.4 Geometry for Changes t
- Page 71 and 72:
62Table 3.8 Orbital Characteristics
- Page 73 and 74:
64The six satellite subset demonstr
- Page 75 and 76:
6625874U SRS-3a (km) 8132.08 8132.0
- Page 77 and 78:
68Figure 3.6 Rendezvous of SRS with
- Page 79 and 80:
7010.90.80.70.60.50.40.30.20.102516
- Page 81 and 82:
72Table 3.17 Classical Orbital Elem
- Page 83 and 84:
74Table 3.19 Classical Orbital Elem
- Page 85:
76Figure 3.12 Rendezvous of SRS wit
- Page 88 and 89:
79In our the methodology developmen
- Page 90 and 91:
81(3.12)( ) √ () (3.13)( )8. Calc
- Page 92 and 93:
83and the assumed specific impulse
- Page 94 and 95:
̇̇85In order to translate these i
- Page 96 and 97:
87CHAPTER 4CONCLUSIONS AND RECOMMEN
- Page 98 and 99:
89REFERENCES1. Rodriguez H.M., Liou
- Page 100 and 101:
9122. Nishida S., Kawamoto S., Okaw
- Page 102 and 103:
93⃗ ⃗ ⃗ , i, j =1,2,3,…,n (
- Page 104 and 105:
95equation Equation ( A.11), govern
- Page 106 and 107:
Figure A.3 Spacecraft Velocity Comp
- Page 108 and 109:
99A vectoral approach was used to i
- Page 110 and 111:
101lost track of where the orbiting
- Page 112 and 113:
103⁄⁄( ) ( )(A.30)Obviously we
- Page 114 and 115:
̇105where the unit vectors rotate
- Page 116 and 117:
107Argument of periapsis (ω) is th
- Page 118:
109VITAGOKSEL GURGENBURANFormatted: