The Multiobjective Trajectory Optimization for Hypersonic Glide Vehicle Based on Normal Boundary Intersection Method

Figure 5

Trajectory parameters of the minimum peak heat trajectory and maximum terminal range trajectory in Pareto optimal solution.

(a) Altitude-time curve

(b) Speed-time curve

(c) Range-time curve

(d) Peak heat-time curve

(e) Angle of attack-time curve

(f) Angle of bank-time curve