Receding Horizon Trajectory Optimization with Terminal Impact Specifications

Table 1

Case configurations without inequality constraints.

Missile	(𝑋0,𝑌0) (km)	𝛾0 (deg)	𝛾𝑓 (deg)	𝑡𝑓 (s)
1	(−3.5, 8.5)	0	−105	50
2	(−9, −4.5)	45	0	50