Research Article

Steady Glide Dynamic Modeling and Trajectory Optimization for High Lift-to-Drag Ratio Reentry Vehicle

Table 5

Final errors for various integral trajectories.

CasesAltitude (m)Velocity (m/s)Flight path angle (deg.)Longitude (deg.)Latitude (deg.)

Case  0.28580.1398−0.0010260.0027420.002329
Case 2.51930.17140.0018470.0020070.001763
Case 1.38200.1538−0.0018580.0027720.001763
Case 2.18760.00580.0014110.0004520.001763
Case −1.11730.1686−0.0030060.0025340.001690