RENDEZVOUS AND DOCKING OF SPACECRAFT - ESA

IMPULSIVE TRAJECTORIESTANGENTIAL MANOEUVRESRADIAL MANOEUVRESX (V−bar)∆ x = _4ω ∆Vz1X (V−bar)∆Vx1∆ x = 6 πω ∆ Vx1∆Vx2∆Vz∆ z = _ 1ω ∆Vz∆Vz2 11Z (R−bar)∆Vx2Z (R−bar)fly−around toR−bar approachon −R−bar sideX (V−bar)∆Vx1∆ x = 3 _ω π ∆Vx1∆ z = _ 4 ω ∆ Vx1∆Vx1X (V−bar)∆ z = _ 1ω ∆Vz1∆ x = _2ω ∆Vz1∆Vz1Z (R−bar)∆Vx2fly−around toR−bar approachon +R−bar sideZ (R−bar)∆VxDr. W. Fehse – Introduction to RVD – From Ground to Capture – Version 200923