Embedded and validated control algorithms for the spacecraft rendezvous
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![Figure 2.4 – Example of “football” orbit not centered at the target spacecraft (source [ 106 ], Fig](https://thumb-eu.123doks.com/thumbv2/123doknet/2103896.7761/52.892.175.698.692.984/figure-example-football-orbit-centered-target-spacecraft-source.webp)
![Figure 2.5 – Relative trajectories satisfying safety and visibility constraints (source [ 33 ], Fig](https://thumb-eu.123doks.com/thumbv2/123doknet/2103896.7761/53.892.133.788.99.549/figure-relative-trajectories-satisfying-safety-visibility-constraints-source.webp)
![Table 2.1 – Scenarios Parameters a [m] e ν 1 [rad] ∆ν [rad] N ∆V [m/s] 6777280 0.00039 π π {2 5 2 Initial states [m,m/s] X 01 pν 1 q “ r 400, 300, ´40, 0, 0, 0s T X 02 pν 1 q “ r ´800, 600, 200, 0, 0, 0s T X 03 pν 1 q “ r ´1500, 1300, 150, 0, 0, 0s T X 04 pν 1 q “ r 5000, 1300, 500, 0, 0, 0s T Space constraints [m] x “ 50, x “ 150, y “ ´25, y “ 25, z “ ´25, z “ 25](https://thumb-eu.123doks.com/thumbv2/123doknet/2103896.7761/69.892.239.662.247.514/table-scenarios-parameters-initial-states-pn-space-constraints.webp)
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