Optimal Ascent Guidance for Air-Breathing Launch Vehicle Based on Optimal Trajectory Correction

Table 1

Initial and required final states of the vehicle.

𝑟ini (m)	𝑣ini (m/s)	𝛾ini (deg)	𝑟𝑟𝑓 (m)	𝑣𝑟𝑓 (m/s)	𝛾𝑟𝑓 (deg)
20000	1000	0	35000	2000	0