Research Article

Boost-Phase Trajectory Planning with the Nonregular Reachable Area Constraints

Table 10

Results of model uncertainty and disturbances.

ItemMaximum energyMinimum energy

Terminal deviationHeight (m)500.00.0
Velocity (m/s)0.0-71.0
Flight path angle (°)0.00.0
Heading angle (°)0.00.0
Performance indexMaximum range (km)996.0978.5
Path constraintsMaximum attack angle (°)20.020.0
Maximum change rate of attack angle (°/s)10.010.0
Maximum sideslip angle (°)10.010.0
Maximum change rate of sideslip angle (°/s)5.02.8
TimelinessCalculation time (s)8.614.9