Research Article
PySCP: A Multiple-Phase Optimal Control Software Using Sequential Convex Programming
Table 4
Boundary conditions of the flight mission.
| State variables | Initial condition | Final condition |
| Altitude (km) | 0 | 500 | Downrange (km) | 0 | [2000, 5000] | Velocity (km) | 50 | 7905 | Flight path angle (deg) | [85, 90] | 0 |
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